Systems, apparatus, methods, and computer program products for stabilized aeronautical operating interface components

Abstract

The present disclosure relates to systems, apparatuses, methods, and computer program products for stabilized aeronautical operating interface components. Systems, apparatuses, methods, and computer program products are provided herein. For example, a method may include receiving aviation operation display data associated with an aircraft. In some embodiments, the method includes capturing aviation operation impact data using one or more aircraft components of the aircraft. In some embodiments, the aeronautical operational impact data is indicative of aeronautical instability events. In some embodiments, the method includes generating aeronautical stability adjustment data by applying the aeronautical operational impact data to an aeronautical stability adjustment model. In some embodiments, the method includes generating a stabilized aeronautical operation interface component based on the aeronautical stability adjustment data and the aeronautical operation display data. In some embodiments, the method includes causing the stabilized aeronautical operating interface component to be presented to an aeronautical operating interface of a device.

Description

[0001] Cross Reference to Related Applications

[0002] This application claims the benefit of U.S. Provisional Patent Application No. 63 / 593,860, filed October 27, 2023, and Indian Provisional Patent Application No. 202411054939, filed July 18, 2024, the entire contents of both of which are incorporated herein by reference. TECHNICAL FIELD

[0003] Embodiments of the present disclosure generally relate to systems, devices, methods, and computer program products for a stabilized aviation operating interface component. BACKGROUND

[0004] Applicants have recognized numerous technical challenges and difficulties associated with unstable aviation interface components. Through exertions of effort, wisdom, and innovation, Applicants have solved problems associated with unstable aviation interface components by developing solutions embodied in the present disclosure, which will be described in detail below. SUMMARY

[0005] Various embodiments described herein relate to systems, devices, methods, and computer program products for a stabilized aviation operating interface component.

[0006] According to one aspect of the present disclosure, a method is provided. In some embodiments, the method includes receiving aviation operating display data associated with an aircraft. In some embodiments, the method includes capturing aviation operating impact data using one or more aircraft components of the aircraft. In some embodiments, the aviation operating impact data is indicative of an aviation instability event. In some embodiments, the method includes generating aviation stability adjustment data by applying the aviation operating impact data to an aviation stability adjustment model. In some embodiments, the method includes generating a stabilized aviation operating interface component based on the aviation stability adjustment data and the aviation operating display data. In some embodiments, the stabilized aviation operating interface component includes one or more stabilized aviation operating display items. In some embodiments, the method includes causing the stabilized aviation operating interface component to be presented to an aviation operating interface of a device.

[0007] In some embodiments, the aviation operating interface includes one or more touch zones.

[0008] In some embodiments, the stabilized aviation operating interface component includes one or more remapped touch zones.

[0009] In some embodiments, the method includes identifying predicted aviation operating impact data.

[0010] In some embodiments, the method includes determining, based on the predicted aviation operation impact data, that the aircraft is predicted to be affected by an aviation instability event.

[0011] In some embodiments, the method includes identifying aviation operation data.

[0012] In some embodiments, the method includes generating, based on the aviation operation data, an aviation operation interface component.

[0013] In some embodiments, the aviation operation interface component includes one or more aviation operation display items.

[0014] In some embodiments, the method includes causing the aviation operation interface component to be presented on an aviation operation interface.

[0015] In some embodiments, the aviation instability event is one or more of a landing associated with the aircraft, a takeoff associated with the aircraft, weather associated with the aircraft, or turbulence associated with the aircraft.

[0016] In some embodiments, the aviation operation impact data is captured while the aircraft is performing an aviation mission.

[0017] In some embodiments, the device is a flight management system, an electronic flight bag, or a multifunction control and display unit.

[0018] In some embodiments, the device is physically secured to the aircraft.

[0019] In some embodiments, the aviation stability adjustment data represents an estimated position change of an eye gaze of an operator of the aircraft.

[0020] In some embodiments, the aviation stability adjustment data represents an estimated position change of the device.

[0021] According to another aspect of the disclosure, an apparatus is provided. In some embodiments, the apparatus includes a memory and one or more processors communicatively coupled to the memory. In some embodiments, the one or more processors are configured to receive aerial operations display data associated with an aerial vehicle. In some embodiments, the one or more processors are configured to capture aerial operations impact data using one or more aerial vehicle components of the aerial vehicle. In some embodiments, the aerial operations impact data is indicative of an aerial instability event. In some embodiments, the one or more processors are configured to generate aerial stability adjustment data by applying the aerial operations impact data to an aerial stability adjustment model. In some embodiments, the one or more processors are configured to generate a stable aerial operations interface component based on the aerial stability adjustment data and the aerial operations display data. In some embodiments, the stable aerial operations interface component includes one or more stable aerial operations display items. In some embodiments, the one or more processors are configured to cause the stable aerial operations interface component to be presented to an aerial operations interface of a device.

[0022] In some embodiments, the aerial operations interface includes one or more touch zones.

[0023] In some embodiments, the stable aerial operations interface component includes one or more remapped touch zones.

[0024] In some embodiments, the one or more processors are configured to identify predicted aerial operations impact data.

[0025] In some embodiments, the one or more processors are configured to determine, based on the predicted aerial operations impact data, that the aerial vehicle is predicted to be affected by an aerial instability event.

[0026] In some embodiments, the one or more processors are configured to identify aerial operations data.

[0027] In some embodiments, the one or more processors are configured to generate an aerial operations interface component based on the aerial operations data.

[0028] In some embodiments, the aerial operations interface component includes one or more aerial operations display items.

[0029] In some embodiments, the one or more processors are configured to cause the aerial operations interface component to be presented on an aerial operations interface.

[0030] In some embodiments, the aerial instability event is one or more of a landing associated with the aerial vehicle, a takeoff associated with the aerial vehicle, weather associated with the aerial vehicle, or turbulence associated with the aerial vehicle.

[0031] In some embodiments, the device is a flight management system, electronic flight bag, or multifunction control and display unit.

[0032] In some embodiments, the aviation stability adjustment data represents an estimated change in position of an eye gaze of an operator of the aircraft.

[0033] According to another aspect of the disclosure, a computer program product is provided. In some embodiments, the computer program product includes at least one non-transitory computer-readable storage medium having computer program code stored thereon. In some embodiments, the computer program code, when executed with at least one processor, configures the computer program product to receive aviation operation display data associated with an aircraft. In some embodiments, the computer program code, when executed with at least one processor, configures the computer program product to capture aviation operation impact data using one or more aircraft components of the aircraft. In some embodiments, the aviation operation impact data is indicative of an aviation instability event. In some embodiments, the computer program code, when executed with at least one processor, configures the computer program product to generate aviation stability adjustment data by applying the aviation operation impact data to an aviation stability adjustment model. In some embodiments, the computer program code, when executed with at least one processor, configures the computer program product to generate a stable aviation operation interface component based on the aviation stability adjustment data and the aviation operation display data. In some embodiments, the stable aviation operation interface component includes one or more stable aviation operation display items. In some embodiments, the computer program code, when executed with at least one processor, configures the computer program product to cause the stable aviation operation interface component to be presented to an aviation operation interface of a device. BRIEF DESCRIPTION OF DRAWINGS

[0034] Reference will now be made to the drawings. Components shown in the drawings can or can not be present in certain embodiments described herein. Some embodiments can include fewer (or more) than those shown in the drawings.

[0035] Figure 1 An example block diagram illustrating an environment in which embodiments of the disclosure can operate is shown;

[0036] Figure 2 An example block diagram illustrating an example apparatus that can be specially configured according to example embodiments of the disclosure is shown;

[0037] Figure 3 Example interface components according to one or more embodiments of the disclosure are shown;

[0038] Figure 4 An example interface component is shown in accordance with one or more embodiments of the present disclosure;

[0039] Figure 5 A flow diagram of an example method is shown in accordance with one or more embodiments of the present disclosure; and

[0040] Figure 6 A flow diagram of an example method is shown in accordance with one or more embodiments of the present disclosure. DETAILED DESCRIPTION

[0041] Some embodiments of the present disclosure will now be described with reference to the attached figures, which are presented for the purpose of illustrating one or more embodiments of the present disclosure and not for the purpose of limiting the same. In fact, the various embodiments of the present disclosure can be embodied in many different forms and should not be construed as limited to the embodiments set forth herein; rather, these embodiments are provided so that this disclosure will satisfy applicable legal requirements. Throughout the disclosure, like reference numerals refer to like elements in which:

[0042] As used herein, the term “includes” means includes but not limited to, and is to be construed in the same manner as “comprising” in the specification. The use of broader terms such as “includes,” “comprises,” and “having” should be understood in the same manner as “comprising” when used in the specification.

[0043] The phrases “in one embodiment,” “according to one embodiment,” “in some embodiments,” and the like generally mean the particular feature, structure, or characteristic following the phrase is included in at least one embodiment of the present disclosure, and can be included in more than one embodiment of the present disclosure (importantly, such phrases are not necessarily referring to the same embodiment).

[0044] The words “example” or “exemplary” are used herein to mean “serving as an example, instance, or illustration.” Any implementation described herein as “exemplary” is not necessarily to be construed as preferred or advantageous over other implementations.

[0045] If the specification states a component, feature, structure, or characteristic “may,” “could,” “should,” “would,” “can,” “likely,” “typically,” “optionally,” “for example,” “usually,” or “possibly” (or other similar language) be included or have a characteristic, that particular component, feature, structure, or characteristic is not required to be included or to have the characteristic. Such components, features, structures, or characteristics can be optionally included in some embodiments or can be excluded.

[0046] Use of the term“circuitry” as used herein with respect to components of systems or devices should be understood to include specific hardware configured to perform the functions associated with the particular circuitry as described herein. The term“circuitry” should be interpreted broadly to encompass both a purely hardware circuit and a hardware and software circuit. For example, in some embodiments, “circuitry” can include processing circuitry, communication circuitry, input / output circuitry, etc. In some embodiments, other elements can provide or supplement the functionality of a particular circuitry. Alternatively or additionally, in some embodiments, other elements of the systems and / or devices described herein can provide or supplement the functionality of another particular circuitry group. For example, a processor can provide processing functionality to any of the circuitry groups, a memory can provide storage functionality to any of the circuitry groups, a communication circuitry can provide network interface functionality to any of the circuitry groups, etc.

[0047] SUMMARY

[0048] Example embodiments disclosed herein address technical problems associated with unstable aviation interface assemblies. As will be appreciated by those skilled in the art to which this disclosure pertains, there are many example scenarios in which an aviation interface assembly can be desired.

[0049] In many applications, it can be desirable to use an aviation interface assembly, such as an aviation interface assembly associated with a flight management system of an aircraft. For example, it can be desirable to use an aviation interface assembly to facilitate an aviation mission associated with an aircraft (e.g., moving from one airport to another) in a safe, efficient, and accurate manner. In some implementations, the aviation interface assembly and / or the aircraft associated with the aviation interface assembly is affected by an aviation instability event. For example, the aviation interface assembly and / or the aircraft associated with the aviation interface assembly can be affected by aviation instability events including weather, turbulence, landing, takeoff, etc.

[0050] In some implementations, an aviation instability event can reduce the usefulness of an aviation interface component because the aviation interface component becomes unstable (e.g., the aviation interface component can shake due to the aviation instability event). For example, an aviation instability event can cause an aviation interface component to become unstable such that information displayed on the aviation interface component cannot be read by an operator of the aircraft (e.g., a pilot). As another example, an aviation instability event can cause an aviation interface component to become unstable such that an operator of the aircraft cannot use the aviation interface component to perform an aviation task (e.g., cause the aircraft to change altitude). As another example, an aviation instability event can cause an aviation interface component to become unstable such that an operator of the aircraft is affected by motion sickness due to the shaking of the aviation interface component. Accordingly, there is a need for systems, apparatuses, methods, and computer program products for generating a stable aviation operating interface even when an aviation interface component and / or an aircraft are affected by an aviation instability event.

[0051] Accordingly, to address these and / or other issues related to aviation interface components, example systems, apparatus, methods, and computer program products for generating a stable aviation operating interface component are disclosed herein. For example, embodiments of the present disclosure described in greater detail below include a method that includes receiving aviation operating display data associated with an aircraft. In some embodiments, the method includes capturing aviation operating impact data using one or more aircraft components of the aircraft. In some embodiments, the aviation operating impact data is indicative of an aviation instability event. In some embodiments, the method includes generating aviation stability adjustment data by applying the aviation operating impact data to an aviation stability adjustment model. In some embodiments, the method includes generating a stable aviation operating interface component based on the aviation stability adjustment data and the aviation operating display data. In some embodiments, the method includes causing the stable aviation operating interface component to be presented to an aviation operating interface of a device. Accordingly, the systems, apparatus, methods, and computer program products for a stable aviation operating interface component provided herein enable a stable aviation operating interface even when an aviation interface component and / or an aircraft are affected by an aviation instability event.

[0052] Example systems and apparatus

[0053] Embodiments of the present disclosure herein include systems, apparatus, methods, and computer program products configured for generating a stable aviation operating interface component. It should be readily appreciated that embodiments of the apparatus, systems, methods, and computer program products described herein can be configured in various additional and alternative manners other than those expressly described herein.

[0054] Figure 1An example block diagram illustrating an environment 100 in which embodiments of the present disclosure can operate is shown. Specifically, Figure 1 A flying vehicle 110 is shown. In some embodiments, the flying vehicle 110 can describe any machine, robot, computing device, and / or apparatus constructed of hardware, software, firmware, and / or any combination thereof that is maneuvered throughout an environment by a medium, such as air. In some cases, the flying vehicle 110 is used to transport objects, entities (e.g., people, animals, or other living beings), and / or other on-board cargo. In some cases, the flying vehicle 110 can not transport objects other than the flying vehicle itself. Examples of the flying vehicle 110 include an airplane, a helicopter, a drone, and the like. In some embodiments, the flying vehicle 110 is not limited to the examples listed herein and can include other types of transportation devices.

[0055] In some embodiments, the flying vehicle 110 is configured to perform an aviation mission. In some embodiments, an aviation mission is a defined series of operations performed by the flying vehicle 110. For example, can include a defined series of operations performed by the flying vehicle 110 for moving from a first airport to a second airport. In this regard, in some embodiments, an aviation mission can include a defined series of operations performed by the flying vehicle 110 including operations performed while the flying vehicle 110 performs pre-flight procedures (e.g., at a gate before a flight), leaves the gate, taxis, takes off, in-flight, lands, parks at a gate, and performs post-flight procedures (e.g., at a gate after a flight ends), and the like. For example, an aviation mission can include a defined series of operations including leaving a gate at a first airport, taxiing to a runway at the first airport (e.g., a departure airport), taking off from the first airport, flying to a second airport (e.g., a destination airport), landing at the second airport, taxiing to a gate at the second airport, and parking at the gate at the second airport.

[0056] In some embodiments, the flying vehicle 110 is associated with a determinable location. In some embodiments, the determinable location of the flying vehicle 110 represents an absolute location (e.g., GPS coordinates, latitude and longitude location, address, and the like) or a relative location (e.g., an identifier representing a location of the flying vehicle 110 relative to one or more other flying vehicles, one or more buildings (e.g., airports), corporate headquarters, or a general description in the world (e.g., based at least in part on a continent, country, ocean, or other definable region)). In some embodiments, the flying vehicle 110 includes and / or is otherwise associated with a location sensor and / or a software-driven location service that provides location data corresponding to the flying vehicle 110. In other embodiments, the location of the flying vehicle 110 is stored and / or otherwise determinable to one or more systems.

[0057] In some embodiments, the environment 100 includes an external aviation stability device 140. In some embodiments, the external aviation stability device 140 is electronically and / or communicatively coupled to the aircraft 110, the onboard aviation stability device 180, the one or more aircraft components 130, and / or the one or more databases 170. The external aviation stability device 140 can be located remotely from the aircraft 110. In this regard, for example, the external aviation stability device 140 can be located in a remote cloud server and is electronically and / or communicatively coupled to the aircraft 110, the onboard aviation stability device 180, the one or more aircraft components 130, and / or the one or more databases 170 via the network 150. In some embodiments, the external aviation stability device 140 is configured via hardware, software, firmware, and / or a combination thereof to perform data ingestion of one or more types of data, such as aviation operation data, aviation operation display data, aviation operation impact data, predicted aviation operation impact data, aviation stability adjustment data, and the like.

[0058] Additionally or alternatively, in some embodiments, the external aviation stability device 140 is configured via hardware, software, firmware, and / or a combination thereof to generate and / or transmit commands that control, adjust, or otherwise affect the operation of one or more of the aircraft 110, the onboard aviation stability device 180, the one or more aircraft components 130, and / or the one or more databases 170. For example, the external aviation stability device 140 can be configured to generate a stabilized aviation operation interface component. Additionally or alternatively, in some embodiments, the external aviation stability device 140 is configured via hardware, software, firmware, and / or a combination thereof to perform data reporting, provide data, and / or other data output processes associated with monitoring or otherwise analyzing the operation of one or more of the aircraft 110, the onboard aviation stability device 180, the one or more aircraft components 130, and / or the one or more databases 170. For example, in various embodiments, the external aviation stability device 140 can be configured to implement and / or perform one or more operations and / or functions described herein.

[0059] In some embodiments, the environment 100 includes an onboard aviation stability device 180. In some embodiments, the onboard aviation stability device 180 is electronically and / or communicatively coupled to the aircraft 110, the external aviation stability device 140, the one or more aircraft components 130, and / or the one or more databases 170. The onboard aviation stability device 180 can be located within the aircraft 110. In some embodiments, the onboard aviation stability device 180 is a flight management system (FMS). For example, the onboard aviation stability device 180 can be a connected flight management system (CFMS).

[0060] Additionally or alternatively, the onboard aviation stabilization device 180 is an electronic flight bag (EFB). In some embodiments, the onboard aviation stabilization device 180 is physically affixed to the aircraft 110. For example, the onboard aviation stabilization device 180 can be a built-in component of the aircraft 110 that is permanently affixed to the aircraft 110 (e.g., when the onboard aviation stabilization device 180 is a flight management system (FMS)). As another example, the onboard aviation stabilization device 180 can be a built-in component of the aircraft 110 that is temporarily affixed to the aircraft 110 (e.g., when the onboard aviation stabilization device 180 is an electronic flight bag). In some embodiments, the onboard aviation stabilization device 180 is configured via hardware, software, firmware, and / or a combination thereof to perform data ingestion of one or more types of data, such as aviation operations data, aviation operations display data, aviation operations impact data, predicted aviation operations impact data, aviation stabilization adjustment data, and the like.

[0061] Additionally or alternatively, in some embodiments, the onboard aviation stability device 180 is configured, via hardware, software, firmware, and / or a combination thereof, to generate and / or transmit commands that control, adjust, or otherwise influence the operation of one or more of the aircraft 110, the external aviation stability device 140, the one or more aircraft components 130, and / or the one or more databases 170. For example, the onboard aviation stability device 180 can be configured to generate a stable aviation operations interface component. Additionally or alternatively, in some embodiments, the onboard aviation stability device 180 is configured, via hardware, software, firmware, and / or a combination thereof, to perform data reporting, provide data, and / or other data output processes associated with monitoring or otherwise analyzing the operation of one or more of the aircraft 110, the external aviation stability device 140, the one or more aircraft components 130, and / or the one or more databases 170. For example, in various embodiments, the onboard aviation stability device 180 can be configured to implement and / or perform one or more operations and / or functions described herein. In some embodiments, the environment 100 includes one or more aircraft components 130. In some embodiments, the one or more aircraft components 130 are electronically and / or communicatively coupled to the aircraft 110, the external aviation stability device 140, the onboard aviation stability device 180, and / or the one or more databases 170. The one or more aircraft components 130 can be located within the aircraft 110. In this regard, for example, the one or more aircraft components 130 can be one or more individual components of the aircraft 110 that perform a particular function during operation of the aircraft 110. For example, the one or more aircraft components 130 can include one or more of a multifunction control and display unit (MCDU), a flight management system (FMS) (e.g., a secondary flight management system when the onboard aviation stability device 180 is a flight management system), an inertial reference system (IRS), a global positioning system (GPS), a sensor, an actuator, a primary flight display, a radar (e.g., a weather radar, a millimeter wave-based radar, etc.), an engine, an auxiliary power unit (APU), an enhanced ground proximity warning system (EGPWS), a landing gear, a flap, a power supply, an aileron, an autopilot system, a tail, a camera (cockpit camera), an inertial measurement unit (IMU), a gyroscope, an accelerometer, a super-tachometer, a display processor, an LRU, etc. In this regard, for example, individual components of the aircraft 110 can include components associated with a particular process or operation performed by the aircraft 110. In some embodiments, the one or more aircraft components 130 are physically secured to the aircraft 110. In some embodiments, the one or more aircraft components 130 include the onboard aviation stability device 180.In some embodiments, one or more aircraft components 130 are configured via hardware, software, firmware, and / or combinations thereof to perform data ingestion of one or more types of data, such as aerial operation data, aerial operation display data, aerial operation impact data, predicted aerial operation impact data, aerial stability adjustment data, and the like.

[0062] Additionally or alternatively, in some embodiments, one or more aircraft components 130 are configured via hardware, software, firmware, and / or combinations thereof to generate and / or transmit commands that control, adjust, or otherwise affect the operation of one or more of the aircraft 110, the external aerial stability device 140, the onboard aerial stability device 180, and / or the one or more databases 170. For example, one or more aircraft components 130 can be configured to determine aerial mission impacts. Additionally or alternatively, in some embodiments, one or more aircraft components 130 are configured via hardware, software, firmware, and / or combinations thereof to perform data reporting, provide data, and / or other data output processes associated with monitoring or otherwise analyzing the operation of one or more of the aircraft 110, the external aerial stability device 140, the onboard aerial stability device 180, and / or the one or more databases 170. For example, in various embodiments, one or more aircraft components 130 can be configured to implement and / or perform one or more operations and / or functions described herein.

[0063] In some embodiments, the onboard aerial stability device 180 and / or the external aerial stability device 140 are configured to cause actuation of one or more of the one or more aircraft components 130. For example, the onboard aerial stability device 180 and / or the external aerial stability device 140 can be configured to cause actuation of one or more of the one or more aircraft components 130 based on aerial operation data, aerial operation display data, aerial operation impact data, predicted aerial operation impact data, aerial stability adjustment data, and the like.

[0064] In some embodiments, the environment 100 includes one or more databases 170. The one or more databases 170 can be configured to receive, store, and / or transmit data. For example, the one or more databases 170 can be configured to receive, store, and / or transmit data associated with the aircraft 110, the external aerial stability device 140, the one or more aircraft components 130, and / or the onboard aerial stability device 180. In this regard, for example, the one or more databases 170 can be configured to receive, store, and / or transmit aerial operation data, aerial operation display data, aerial operation impact data, predicted aerial operation impact data, aerial stability adjustment data, and / or the like. The one or more databases 170 can be positioned remotely from the aircraft 110, proximate to the aircraft 110, and / or within the aircraft 110.

[0065] The network 150 can be embodied in any of myriad network configurations. In some embodiments, the network 150 can be a public network (e.g., the Internet). In some embodiments, the network 150 can be a private network (e.g., an internal localized or closed network between particular devices). In some other embodiments, the network 150 can be a hybrid network (e.g., a network that enables internal communication between devices that are capable of particular connections and external communication with other devices). In various embodiments, the network 150 can include one or more base stations, relays, routers, switches, cell towers, communication cables, routing stations, and / or the like. In various embodiments, the components of the environment 100 can be communicatively coupled to transmit data to and / or receive data from one another over the network 150. Such configurations include, but are not limited to, wired or wireless personal area networks (PANs), local area networks (LANs), metropolitan area networks (MANs), wide area networks (WANs), and / or the like.

[0066] Further, while Figure 1 While certain components are shown as separate, independent entities communicating over the network 150, the various embodiments are not limited to this configuration. In other embodiments, one or more components can be directly connected and / or shared hardware, etc. For example, in some embodiments, the external aerial stability device 140 can include the one or more databases 170.

[0067] Figure 2 An example block diagram of an example apparatus that can be specially configured in accordance with example embodiments of the present disclosure is shown. Specifically, Figure 2An example computing device 200 (“device 200”) configured specifically in accordance with at least some example embodiments of the present disclosure is depicted. For example, the computing device 200 can be embodied as one or more of a specially configured personal computing device, a specially configured cloud-based computing device, a specially configured embedded computing device (e.g., configured for edge computing, etc.). Examples of the device 200 can include, but are not limited to, the external aerial stabilization device 140, the one or more aircraft components 130, the one or more databases 170, and / or the onboard aerial stabilization device 180. The device 200 includes a processor 202, a memory 204, input / output circuitry 206, communication circuitry 208, and / or optional artificial intelligence (“AI”) and machine learning circuitry 210. In some embodiments, the device 200 is configured to implement and perform the operations described herein.

[0068] While components are described with respect to functional limitations, it should be understood that a particular implementation necessarily includes the use of particular computing hardware. It should also be understood that, in some embodiments, certain of the components described herein include similar or common hardware. For example, in some embodiments, both circuitry groups utilize the use of the same processor, memory, circuitry, etc. to perform their associated functions, such that each circuitry group does not require duplicative hardware.

[0069] In various embodiments, the computing device 200, such as the external aerial stabilization device 140, the one or more aircraft components 130, the one or more databases 170, and / or the onboard aerial stabilization device 180, can refer to, for example, one or more computers, computing entities, desktop computers, mobile phones, tablet computers, phablets, notebooks, laptops, distributed systems, servers, etc., and / or any combination of devices or entities suitable for performing the functions, operations, and / or processes described herein. Such functions, operations, and / or processes can include, for example, transmitting, receiving, operating, processing, displaying, storing, determining, creating / generating, monitoring, evaluating, comparing, and / or similar terms that can be used herein. In one embodiment, these functions, operations, and / or processes can be performed on data, content, information, and / or similar terms that can be used herein. In this regard, as described herein, the device 200 embodies a specially configured particular computing entity that is transformed to implement the particular operations described herein and provide the particular advantages associated therewith.

[0070] The processor 202, or processor circuit 202, can be embodied in a number of different ways. In various embodiments, the use of the term“processor” should not be construed to refer exclusively to internal hardware components of the device 200. In fact, in some example embodiments, the processor 202 can include one or more processing devices that are independent of the device 200, or one or more processing devices that are external to the device 200. In some example embodiments, the processor 202 can include one or more processing devices that are configured to execute independently. Alternatively or additionally, the processor 202 can include one or more processors that are configured in a serial, bus, or other configuration to enable independent execution of operations, instructions, pipelines, and / or multithreading.

[0071] In example embodiments, the processor 202 can be configured to execute instructions stored in the memory 204 or otherwise accessible to the processor. Alternatively or additionally, the processor 202 can be configured to execute hard coded functionality. Thus, whether configured by hardware or software methods, or by a combination thereof, the processor 202 can represent an entity capable of performing operations according to embodiments of the present disclosure while configured accordingly. Alternatively or additionally, the processor 202 can be embodied as a

[0072] In some embodiments, the processor 202 (and / or a co-processor, or any other processing circuitry that assists the processor or is otherwise associated with the processor) communicates with the memory 204 via a bus for passing information among the components of the device 200.

[0073] The memory 204, or memory circuit 204, can be non-transitory and can include, for example, one or more volatile memory devices and / or non-volatile memory devices. In some embodiments, the memory 204 includes or embodies electronic storage devices (e.g., computer readable storage medium). In some embodiments, the memory 204 is configured to store information, data, content, applications, instructions, etc. for use by the device 200 in implementing various operations and / or functions in accordance with example embodiments of the present disclosure.

[0074] Input / output circuitry 206 can be included in the device 200. In some embodiments, the input / output circuitry 206 can provide output and / or receive input to the user. The input / output circuitry 206 can be in communication with the processor 202 to provide such functionality. The input / output circuitry 206 can include one or more user interfaces. In some embodiments, the user interface can include a display that includes an interface to a web user interface, an application program user interface, a user device, a backend system. In some embodiments, the input / output circuitry 206 also includes a keyboard, a mouse, a joystick, a touch screen, a touch area, soft keys, a microphone, a speaker, or other input / output mechanisms. The processor 202 and / or the input / output circuitry 206 including a processor can be configured to control one or more operations and / or functions of one or more user interface elements through computer program instructions (e.g., software and / or firmware) stored on a memory accessible to the processor (e.g., memory 204, etc.). In some embodiments, the input / output circuitry 206 includes or utilizes a user-facing application program to provide input / output functionality to a computing device and / or other display associated with a user.

[0075] Communication circuitry 208 can be included in the device 200. The communication circuitry 208 can include any means for communicating data from and / or to network and / or any other devices, circuitry, or modules that are in communication with the device 200, such as devices or circuitry embodied in hardware or a combination of hardware and software that are configured to receive and / or transmit data from / to the network. In some embodiments, the communication circuitry 208 includes, for example, a network interface for enabling communications with a wired or wireless communication network. Additionally or alternatively, the communication circuitry 208 can include one or more network interface cards, antennas, buses, switches, routers, modems, and supporting hardware, firmware, and / or software, or any other devices that are suitable for supporting communications via one or more communication networks. In some embodiments, the communication circuitry 208 can include circuitry for interacting with an antenna and / or other hardware or software in order to cause transmission of signals via the antenna and / or to process received signals from the antenna. In some embodiments, the communication circuitry 208 enables transmission and / or reception of data to and / or from user devices, one or more sensors, and / or other external computing devices that are in communication with the device 200.

[0076] Data ingestion circuitry 212 can be included in the apparatus 200. The data ingestion circuitry 212 can include hardware, software, firmware, and / or combinations thereof designed and / or configured to capture, receive, request, and / or otherwise collect data associated with operations of the aircraft 110. In some embodiments, the data ingestion circuitry 212 includes hardware, software, firmware, and / or combinations thereof that communicates with one or more sensor components, etc. within the aircraft 110 to receive particular data associated with such operations of the aircraft 110. Additionally or alternatively, in some embodiments, the data ingestion circuitry 212 includes hardware, software, firmware, and / or combinations thereof that retrieves particular data associated with the aircraft 110 from one or more data repositories accessible to the apparatus 200.

[0077] AI and machine learning circuitry 210 can be included in the apparatus 200. The AI and machine learning circuitry 210 can include hardware, software, firmware, and / or combinations thereof designed and / or configured to request, receive, process, generate, and transmit data, data structures, control signals, and electronic information for training and executing trained AI and machine learning models configured to facilitate the operations and / or functionality described herein. For example, in some embodiments, the AI and machine learning circuitry 210 includes hardware, software, firmware, and / or combinations thereof that identifies training data and / or utilizes such training data to train particular machine learning models, AI, and / or other models to generate particular output data based at least in part on learning from the training data. Additionally or alternatively, in some embodiments, the AI and machine learning circuitry 210 includes hardware, software, firmware, and / or combinations thereof that embodies or retrieves trained machine learning models, AI, and / or other specially configured models for processing input data. Additionally or alternatively, in some embodiments, the AI and machine learning circuitry 210 includes hardware, software, firmware, and / or combinations thereof that processes received data utilizing one or more algorithms, functions, subroutines, etc. in one or more pre-processing and / or subsequent operations that do not require utilization of machine learning or AI models.

[0078] Data output circuitry 214 can be included in the apparatus 200. The data output circuitry 214 can include hardware, software, firmware, and / or combinations thereof that configure and / or generate outputs based at least in part on data processed by the apparatus 200. In some embodiments, the data output circuitry 214 includes hardware, software, firmware, and / or combinations thereof that generate a particular report based at least in part on the processed data, e.g., where the report is generated based at least in part on a particular reporting protocol. Additionally or alternatively, in some embodiments, the data output circuitry 214 includes hardware, software, firmware, and / or combinations thereof that configure particular output data objects, output data files, and / or user interfaces for storage, transmission, and / or display. For example, in some embodiments, the data output circuitry 214 generates and / or specifically configures particular data outputs for transmission to another system subsystem for further processing. Additionally or alternatively, in some embodiments, the data output circuitry 214 includes hardware, software, firmware, and / or combinations thereof that cause a specifically configured user interface to be presented based at least in part on data received and / or processed by the apparatus 200.

[0079] In some embodiments, two or more circuits of the group of circuits 202-214 are combinable. Alternatively or additionally, one or more circuits of the group of circuits 202-214 perform some or all of the operations and / or functionality described herein as being associated with another circuit. In some embodiments, two or more circuits of the group of circuits 202-214 are combined into a single module embodied in hardware, software, firmware, and / or combinations thereof. For example, in some embodiments, one or more circuits of the circuit group (e.g., the AI and machine learning circuit 210) are combinable with the processor 202 such that the processor 202 performs one or more of the operations described herein with respect to the AI and machine learning circuit 210.

[0080] In some embodiments, the external aviation stability device 140 and / or the onboard aviation stability device 180 are configured to identify aviation operational data. In some embodiments, the aviation operational data includes one or more data items that represent and / or indicate one or more aircraft operational items. In some embodiments, the aircraft operational item is an item associated with an aviation mission (e.g., an aviation mission performed by the aircraft 110). In this regard, in some embodiments, the aircraft operational item is a flight plan item. For example, the flight plan item can represent a flight plan that the aircraft 110 is to follow to perform the aviation mission. In some embodiments, the aircraft operational item is an altitude item. For example, the altitude item can represent one or more altitudes at which the aircraft 110 is to operate to perform the aviation mission. In some embodiments, the aircraft operational item is a speed item. For example, the speed item can represent one or more speeds at which the aircraft 110 is to operate to perform the aviation mission.

[0081] In some embodiments, the aircraft operational item is a heading item. For example, the heading item can represent one or more headings that the aircraft 110 is to follow to perform the aviation mission. In some embodiments, the aircraft operational item is a remaining distance item. For example, the remaining distance item can represent a distance that the aircraft 110 needs to travel to perform the aviation mission. In some embodiments, the aircraft operational item is an arrival time item. For example, the arrival time item can represent a time at which the aircraft 110 is to arrive at a destination airport. In some embodiments, the aircraft operational item is a fuel consumption item. For example, the fuel consumption item can represent an amount of fuel that the aircraft 110 has used in performing the aviation mission. In some embodiments, the aircraft operational item is an originating airport item. For example, the originating airport item can represent an airport from which the aircraft 110 originated in the aviation mission.

[0082] In some embodiments, the aircraft operational item is a destination airport item. For example, the destination airport item can represent an airport to which the aircraft 110 is traveling in the aviation mission. In some embodiments, the aircraft operational item is a landing runway item. For example, the landing runway item can represent a runway on which the aircraft 110 is to land in the aviation mission. In some embodiments, the aircraft operational item is a takeoff runway item. For example, the takeoff runway item can represent a runway on which the aircraft 110 is to take off in the aviation mission. In some embodiments, the aircraft operational item is a taxi item. For example, the taxi item can represent a taxi route that is to be used by the aircraft 110 in the aviation mission. In some embodiments, the aircraft operational item is an aircraft type item. For example, the aircraft type item can represent an aircraft type of the aircraft 110.

[0083] In some embodiments, identifying the aerial operation data includes the external aerial stabilization device 140 and / or the onboard aerial stabilization device 180 being configured to receive the aerial operation data. For example, the external aerial stabilization device 140 and / or the onboard aerial stabilization device 180 can be configured to receive the aerial operation data from an operator (e.g., a pilot) of the aerial vehicle 110. As another example, the external aerial stabilization device 140 and / or the onboard aerial stabilization device 180 can be configured to receive the aerial operation data from one or more databases 170. In some embodiments, identifying the aerial operation data includes the external aerial stabilization device 140 and / or the onboard aerial stabilization device 180 being configured to generate the aerial operation data. For example, the external aerial stabilization device 140 and / or the onboard aerial stabilization device 180 can be configured to generate the aerial operation data using one or more aerial vehicle components 130.

[0084] In some embodiments, the external aerial stabilization device 140 and / or the onboard aerial stabilization device 180 is configured to generate the aerial operation interface component 300. In some embodiments, the aerial operation interface component 300 is generated based on the aerial operation data. In this regard, in some embodiments, the aerial operation interface component 300 includes one or more aerial operation display items 304 configured to display one or more aerial operation items. For example, the aerial operation interface component 300 can include one or more aerial operation display items 304 including a flight plan display item, an altitude display item, a speed display item, a heading display item, a remaining distance display item, an arrival time display item, a fuel consumption display item, an origin airport display item, a destination airport display item, a landing runway display item, a takeoff runway display item, a taxi display item, an aerial vehicle type display item, etc. In some embodiments, each of the one or more aerial operation display items 304 is associated with an original display item location on the aerial operation interface component 300. In this regard, for example, the original display item location can be a location on the aerial operation interface component 300 at and / or where the aerial operation display item is displayed on and / or located on the aerial operation interface component 300.

[0085] In some embodiments, the aerial operation interface component 300 includes one or more touch zones 306. In some embodiments, the one or more touch zones 306 are selectable portions of the aerial operation interface component 300. For example, the one or more touch zones 306 can be selected to display information about an aerial operation display item of the one or more aerial operation display items 304. Additionally or alternatively, the one or more touch zones 306 can be configured to control the aerial vehicle 110 and / or one or more aerial vehicle components 130 of the aerial vehicle 110.

[0086] In some embodiments, one or more touch zones 306 are associated with an original touch zone location on the aviation operating interface assembly 300. In this regard, for example, the original touch zone location can be a location on the aviation operating interface assembly 300 at which a touch zone of the one or more touch zones 306 is displayed and / or located on the aviation operating interface assembly 300 (e.g., touch the original touch zone location to select the touch zone).

[0087] In some embodiments, the external aviation stabilization device 140 and / or the onboard aviation stabilization device 180 are configured to cause the aviation operating interface assembly 300 to be presented to the aviation operating interface 302, such as Figure 3 is shown. In some embodiments, the aviation operating interface 302 is disposed on the onboard aviation stabilization device 180 and / or one or more of the aircraft components 130. For example, the aviation operating interface 302 can be disposed on a multifunction control and display unit. In this regard, for example, the aviation operating interface 302 can be provided to an operator (e.g., a pilot) of the aircraft 110 while the aircraft 110 is performing an aviation mission.

[0088] In some embodiments, the external aviation stabilization device 140 and / or the onboard aviation stabilization device 180 are configured to receive aviation operating display data. In some embodiments, the aviation operating display data includes one or more data items that represent and / or indicate the aviation operating interface assembly 300. In this regard, in some embodiments, the aviation operating display data includes one or more data items that represent the one or more aviation operating display items 304. Additionally or alternatively, the aviation operating display data includes one or more data items that represent the one or more touch zones 306.

[0089] In some embodiments, the external aviation stability device 140 and / or the onboard aviation stability device 180 are configured to capture aviation operation impact data. In some embodiments, the aviation operation impact data includes one or more data items that represent and / or indicate an aviation instability event. In this regard, in some embodiments, the aviation instability event is an event that causes an acceleration motion (e.g., motion in the X-axis, Y-axis, and / or Z-axis) and / or an angular motion (e.g., azimuth motion, pitch motion, and / or roll motion) of the aircraft 110. Additionally or alternatively, the aviation instability event is an event that causes an acceleration motion (e.g., motion in the X-axis, Y-axis, and / or Z-axis) and / or an angular motion (e.g., azimuth motion, pitch motion, and / or roll motion) of the onboard aviation stability device 180 and / or one or more of the aircraft components 130 (e.g., an aircraft component on which the aviation operation interface 302 is disposed). Additionally or alternatively, the aviation instability event is an event that causes an acceleration motion (e.g., motion in the X-axis, Y-axis, and / or Z-axis) and / or an angular motion (e.g., azimuth motion, pitch motion, and / or roll motion) of an eye of an operator of the aircraft 110 (e.g., an eye of a pilot).

[0090] In some embodiments, the aviation instability event is a takeoff associated with the aircraft 110. In this regard, for example, the takeoff associated with the aircraft 110 can cause an acceleration motion (e.g., motion in the X-axis, Y-axis, and / or Z-axis) and / or an angular motion (e.g., azimuthal motion, pitch motion, and / or roll motion) of the aircraft 110, the onboard aviation stabilization device 180, one or more of the aircraft components 130, and / or the eyes of an operator of the aircraft 110. In some embodiments, the aviation instability event is a landing associated with the aircraft 110. In this regard, for example, the landing associated with the aircraft 110 can cause an acceleration motion (e.g., motion in the X-axis, Y-axis, and / or Z-axis) and / or an angular motion (e.g., azimuthal motion, pitch motion, and / or roll motion) of the aircraft 110, the onboard aviation stabilization device 180, one or more of the aircraft components 130, and / or the eyes of an operator of the aircraft 110. In some embodiments, the aviation instability event is weather associated with the aircraft 110. In this regard, for example, the weather associated with the aircraft 110 can cause an acceleration motion (e.g., motion in the X-axis, Y-axis, and / or Z-axis) and / or an angular motion (e.g., azimuthal motion, pitch motion, and / or roll motion) of the aircraft 110, the onboard aviation stabilization device 180, one or more of the aircraft components 130, and / or the eyes of an operator of the aircraft 110. In some embodiments, the aviation instability event is turbulence associated with the aircraft 110. In this regard, for example, the turbulence associated with the aircraft 110 can cause an acceleration motion (e.g., motion in the X-axis, Y-axis, and / or Z-axis) and / or an angular motion (e.g., azimuthal motion, pitch motion, and / or roll motion) of the aircraft 110, the onboard aviation stabilization device 180, one or more of the aircraft components 130, and / or the eyes of an operator of the aircraft 110.

[0091] In some embodiments, the external aerial stability device 140 and / or the onboard aerial stability device 180 are configured to capture aerial operation impact data using one or more of the one or more aircraft components 130. For example, the external aerial stability device 140 and / or the onboard aerial stability device 180 can be configured to capture aerial operation impact data using one or more cockpit cameras, inertial measurement units, motion sensors, gyroscopes, accelerometers, etc. Additionally or alternatively, the external aerial stability device 140 and / or the onboard aerial stability device 180 are configured to capture aerial operation impact data using the onboard aerial stability device 180. For example, the external aerial stability device 140 and / or the onboard aerial stability device 180 can be configured to capture aerial operation impact data using an inertial measurement unit associated with the onboard aerial stability device 180.

[0092] In some embodiments, the external aerial stability device 140 and / or the onboard aerial stability device 180 are configured to generate aerial stability adjustment data. In some embodiments, the aerial stability adjustment data includes one or more data items representing and / or indicative of an estimated change in eye gaze of an operator (e.g., a pilot) of the aircraft 110 due to an aerial instability event. Additionally or alternatively, the aerial stability adjustment data includes one or more data items representing and / or indicative of an estimated change in position of the onboard aerial stability device 180 and / or one or more of the one or more aircraft components 130 due to the aerial instability event.

[0093] In some embodiments, the external aviation stability device 140 and / or the onboard aviation stability device 180 are configured to generate aviation stability adjustment data by applying the aviation operation impact data to an aviation stability adjustment model. In some embodiments, the aviation stability adjustment model is a data entity that describes parameters, hyperparameters, and / or defined operations of a rules-based and / or machine learning model configured to generate the aviation stability adjustment data. In this regard, in some embodiments, the aviation stability adjustment model is configured to utilize one or more of any type of machine learning, rules-based, and / or artificial intelligence techniques, including one or more of computer vision techniques, supervised learning (e.g., using user feedback), unsupervised learning, semi-supervised learning, reinforcement learning, computer vision techniques, sequence modeling techniques, language processing techniques, neural network techniques, generative artificial intelligence techniques, filtering techniques, grouping techniques, ranking techniques, trend analysis techniques, correlation analysis techniques, anomaly detection techniques, clustering techniques, etc. In this regard, in some embodiments, the aviation stability adjustment model is configured to determine, using the aviation operation impact data, an estimated change in eye gaze of an operator (e.g., a pilot) of the aircraft 110 due to the aviation instability event. Additionally or alternatively, the aviation stability adjustment model is configured to determine, using the aviation operation impact data, an estimated change in position of the onboard aviation stability device 180 and / or one or more of the one or more aircraft components 130 due to the aviation instability event.

[0094] In some embodiments, the external aviation stability device 140 and / or the onboard aviation stability device 180 are configured to generate a stabilized aviation operation interface component 400. In some embodiments, the stabilized aviation operation interface component 400 is configured to be generated based on the aviation stability adjustment data and / or the aviation operation display data. In this regard, in some embodiments, the stabilized aviation operation interface component 400 includes one or more stabilized aviation operation display items 404 that correspond to the aviation operation display items 304. For example, the stabilized aviation operation interface component 400 can include one or more stabilized aviation operation display items 404 that include a flight plan display item, an altitude item, a speed display item, a heading display item, a remaining distance display item, an arrival time display item, a fuel consumption display item, an origin airport display item, a destination airport display item, a landing runway display item, a takeoff runway display item, a taxi display item, an aircraft type display item, etc.

[0095] In some embodiments, each of the one or more stable aviation operation display items 404 is associated with a stable display item location on the stable aviation operation interface component 400. In this regard, for example, the stable display item location can be a location on the stable aviation operation interface component 400 at which the stable aviation operation display item is displayed on and / or located on the stable aviation operation interface component 400. In some embodiments, the stable display item location can be a different location than the original display item location. In other words, in some embodiments, the stable aviation operation interface component 400 is configured such that when a display item associated with an aircraft operation item is displayed, the estimated location change of the eyes gaze of an operator of the aircraft 110 (e.g., a pilot) and / or the estimated location change of one or more of the onboard aviation stabilization device 180 and / or one or more aircraft components 130 due to the aviation instability event is considered.

[0096] In some embodiments, the stable aviation operation interface component 400 includes one or more remapped touch zones 406. In some embodiments, the one or more remapped touch zones 406 are selectable portions of the stable aviation operation interface component 400. For example, the one or more remapped touch zones 406 can be selected to display information about a stable aviation operation display item of the one or more stable aviation operation display items 404.

[0097] In some embodiments, the one or more remapped touch zones 406 are associated with a remapped touch zone location on the stable aviation operation interface component 400. In this regard, for example, the remapped touch zone location can be a location on the stable aviation operation interface component 400 at which a remapped touch zone of the one or more remapped touch zones 406 is displayed on and / or located on the stable aviation operation interface component 400 (e.g., touch the remapped touch zone location selects the remapped touch zone). In other words, for example, the one or more remapped touch zones 406 can correspond to the one or more touch zones 306, but be located in a different location to address the aviation instability event.

[0098] In some embodiments, the external aviation stabilization device 140 and / or the onboard aviation stabilization device 180 are configured to cause the stable aviation operation interface component 400 to be presented to the aviation operation interface 302, such as Figure 4The stable aviation operation interface component 400 is shown in FIG. 3. In some embodiments, the stable aviation operation interface component 400 is disposed on one or more of the one or more aircraft components 130 in the airborne aviation stabilization device 180. For example, the stable aviation operation interface component 400 can be disposed on a multifunction control and display unit. In this regard, for example, the stable aviation operation interface component 400 can be provided to an operator (e.g., a pilot) of the aircraft 110 while the aircraft 110 is performing an aviation mission.

[0099] In some embodiments, the external aviation stabilization device 140 and / or the airborne aviation stabilization device 180 are configured to identify predicted aviation operation impact data. In some embodiments, the predicted aviation operation impact data includes one or more data items that represent and / or indicate a predicted aviation instability event. In this regard, in some embodiments, the predicted aviation instability event is a predicted event that is predicted to cause an acceleration motion (e.g., motion in the X-axis, Y-axis, and / or Z-axis) and / or an angular motion (e.g., azimuth motion, pitch motion, and / or roll motion) of the aircraft 110. Additionally or alternatively, the predicted aviation instability event is a predicted event that is predicted to cause an acceleration motion (e.g., motion in the X-axis, Y-axis, and / or Z-axis) and / or an angular motion (e.g., azimuth motion, pitch motion, and / or roll motion) of one or more of the one or more aircraft components 130 (e.g., an aircraft component on which the aviation operation interface 302 is disposed). Additionally or alternatively, the predicted aviation instability event is a predicted event that is predicted to cause an acceleration motion (e.g., motion in the X-axis, Y-axis, and / or Z-axis) and / or an angular motion (e.g., azimuth motion, pitch motion, and / or roll motion) of an eye of an operator of the aircraft 110 (e.g., an eye of a pilot).

[0100] In some embodiments, the predicted aviation instability event is a predicted takeoff associated with the aircraft 110. In this regard, for example, the predicted takeoff associated with the aircraft 110 can be predicted to cause an acceleration motion (e.g., motion in the X-axis, Y-axis, and / or Z-axis) and / or an angular motion (e.g., azimuthal motion, pitch motion, and / or roll motion) of the aircraft 110, the onboard aviation stabilization device 180, one or more of the aircraft components 130, and / or an eye of an operator of the aircraft 110. In some embodiments, the predicted aviation instability event is a predicted landing associated with the aircraft 110. In this regard, for example, the predicted landing associated with the aircraft 110 can be predicted to cause an acceleration motion (e.g., motion in the X-axis, Y-axis, and / or Z-axis) and / or an angular motion (e.g., azimuthal motion, pitch motion, and / or roll motion) of the aircraft 110, the onboard aviation stabilization device 180, one or more of the aircraft components 130, and / or an eye of an operator of the aircraft 110. In some embodiments, the predicted aviation instability event is a predicted weather associated with the aircraft 110. In this regard, for example, the predicted weather associated with the aircraft 110 can be predicted to cause an acceleration motion (e.g., motion in the X-axis, Y-axis, and / or Z-axis) and / or an angular motion (e.g., azimuthal motion, pitch motion, and / or roll motion) of the aircraft 110, the onboard aviation stabilization device 180, one or more of the aircraft components 130, and / or an eye of an operator of the aircraft 110. In some embodiments, the predicted aviation instability event is a predicted turbulence associated with the aircraft 110. In this regard, for example, the predicted turbulence associated with the aircraft 110 can be predicted to cause an acceleration motion (e.g., motion in the X-axis, Y-axis, and / or Z-axis) and / or an angular motion (e.g., azimuthal motion, pitch motion, and / or roll motion) of the aircraft 110, the onboard aviation stabilization device 180, one or more of the aircraft components 130, and / or an eye of an operator of the aircraft 110.

[0101] In some embodiments, the external aviation stability device 140 and / or the onboard aviation stability device 180 is configured to determine that the aircraft 110 is predicted to be affected by an aviation instability event based on the predicted aviation operation impact data. In this regard, in some embodiments, the external aviation stability device 140 and / or the onboard aviation stability device 180 is configured to pre-generate aviation stability adjustment data such that a stable aviation operation interface component 400 can be presented once the aircraft 110 is affected by an aviation instability event. In this way, for example, the external aviation stability device 140 and / or the onboard aviation stability device 180 is able to provide a stable interface component (e.g., the stable aviation operation interface component 400) to an operator of the aircraft 110 in a seamless manner.

[0102] Example methods

[0103] Referring now to Figure 5 , a flowchart illustrating an example method 500 is shown. In this regard, Figure 5 operations that can be performed by the external aviation stability device 140, the aircraft 110, the one or more databases 170, the one or more aircraft components 130, and / or the onboard aviation stability device 180 are shown. In some embodiments, the method 500 includes operations for generating and / or causing a stable aviation operation interface component to be presented to an aviation operation interface, as described above. In some embodiments, the example method 500 defines a computer-implemented process that can be executed by any of the devices and / or systems embodied in hardware, software, firmware, and / or combinations thereof, as described herein. In some embodiments, computer program code comprising one or more computer code instructions is stored to at least one non-transitory computer-readable storage medium such that execution of the computer program code initiates execution of the method 500.

[0104] As shown in block 502, the method 500 includes aviation operation display data associated with the aircraft. As described above, in some embodiments, the aviation operation display data includes one or more data items representing and / or indicative of an aviation operation interface component. In this regard, in some embodiments, the aviation operation display data includes one or more data items representing one or more aviation operation display items. Additionally or alternatively, the aviation operation display data includes one or more data items representing one or more touch zones.

[0105] As represented by block 504, the method 500 includes capturing aviation operation impact data using one or more aircraft components of the aircraft. As noted above, in some embodiments, the aviation operation impact data includes one or more data items that represent and / or indicate an aviation instability event. In this regard, in some embodiments, the aviation instability event is an event that causes an acceleration motion (e.g., motion in the X-axis, Y-axis, and / or Z-axis) and / or an angular motion (e.g., azimuth motion, pitch motion, and / or roll motion) of the aircraft. Additionally or alternatively, the aviation instability event is an event that causes an acceleration motion (e.g., motion in the X-axis, Y-axis, and / or Z-axis) and / or an angular motion (e.g., azimuth motion, pitch motion, and / or roll motion) of one or more of the onboard aviation stability devices and / or one or more of the aircraft components (e.g., an aircraft component on which the aviation operation interface is disposed). Additionally or alternatively, the aviation instability event is an event that causes an acceleration motion (e.g., motion in the X-axis, Y-axis, and / or Z-axis) and / or an angular motion (e.g., azimuth motion, pitch motion, and / or roll motion) of an eye of an operator of the aircraft (e.g., an eye of a pilot).

[0106] In some embodiments, the aviation instability event is a takeoff associated with the aircraft. In this regard, for example, the takeoff associated with the aircraft can cause an acceleration motion (e.g., motion in the X-axis, Y-axis, and / or Z-axis) and / or an angular motion (e.g., azimuth motion, pitch motion, and / or roll motion) of the aircraft, the onboard aviation stabilization device, one or more of the one or more aircraft components, and / or the eyes of an operator of the aircraft. In some embodiments, the aviation instability event is a landing associated with the aircraft. In this regard, for example, the landing associated with the aircraft can cause an acceleration motion (e.g., motion in the X-axis, Y-axis, and / or Z-axis) and / or an angular motion (e.g., azimuth motion, pitch motion, and / or roll motion) of the aircraft, the onboard aviation stabilization device, one or more of the one or more aircraft components, and / or the eyes of an operator of the aircraft. In some embodiments, the aviation instability event is weather associated with the aircraft. In this regard, for example, the weather associated with the aircraft can cause an acceleration motion (e.g., motion in the X-axis, Y-axis, and / or Z-axis) and / or an angular motion (e.g., azimuth motion, pitch motion, and / or roll motion) of the aircraft, the onboard aviation stabilization device, one or more of the one or more aircraft components, and / or the eyes of an operator of the aircraft. In some embodiments, the aviation instability event is turbulence associated with the aircraft. In this regard, for example, the turbulence associated with the aircraft can cause an acceleration motion (e.g., motion in the X-axis, Y-axis, and / or Z-axis) and / or an angular motion (e.g., azimuth motion, pitch motion, and / or roll motion) of the aircraft, the onboard aviation stabilization device, one or more of the one or more aircraft components, and / or the eyes of an operator of the aircraft.

[0107] In some embodiments, the external aviation stabilization device and / or the onboard aviation stabilization device is configured to capture the aviation operation influence data using one or more of the one or more aircraft components. For example, the external aviation stabilization device and / or the onboard aviation stabilization device can be configured to capture the aviation operation influence data using one or more cockpit cameras, inertial measurement units, motion sensors, gyroscopes, accelerometers, and / or the like. Additionally or alternatively, the external aviation stabilization device and / or the onboard aviation stabilization device is configured to capture the aviation operation influence data using the onboard aviation stabilization device. For example, the external aviation stabilization device and / or the onboard aviation stabilization device can be configured to capture the aviation operation influence data using an inertial measurement unit associated with the onboard aviation stabilization device.

[0108] As represented by block 506, the method 500 includes generating aviation stability adjustment data by applying the aviation operation impact data to an aviation stability adjustment model. As noted above, in some embodiments, the aviation stability adjustment data includes one or more data items representing and / or indicative of an estimated change in eye gaze of an operator (e.g., pilot) of the aircraft due to the aviation instability event. Additionally or alternatively, the aviation stability adjustment data includes one or more data items representing and / or indicative of an estimated change in position of the onboard aviation stability equipment and / or one or more of the aircraft components due to the aviation instability event.

[0109] In some embodiments, the external aviation stability equipment and / or the onboard aviation stability equipment is configured to generate the aviation stability adjustment data by applying the aviation operation impact data to an aviation stability adjustment model. In some embodiments, the aviation stability adjustment model is a data entity that describes parameters, hyperparameters, and / or defined operations of a rule-based and / or machine learning model configured to generate the aviation stability adjustment data. In this regard, in some embodiments, the aviation stability adjustment model is configured to utilize one or more of any type of machine learning, rule-based, and / or artificial intelligence techniques, including one or more of computer vision techniques, supervised learning (e.g., using user feedback), unsupervised learning, semi-supervised learning, reinforcement learning, computer vision techniques, sequence modeling techniques, language processing techniques, neural network techniques, generative artificial intelligence techniques, filtering techniques, grouping techniques, ranking techniques, trend analysis techniques, correlation analysis techniques, anomaly detection techniques, clustering techniques, etc. In this regard, in some embodiments, the aviation stability adjustment model is configured to determine, using the aviation operation impact data, an estimated change in eye gaze of an operator (e.g., pilot) of the aircraft due to the aviation instability event. Additionally or alternatively, the aviation stability adjustment model is configured to determine, using the aviation operation impact data, an estimated change in position of the onboard aviation stability equipment and / or one or more of the aircraft components due to the aviation instability event.

[0110] As represented by block 508, the method 500 includes generating a stabilized aviation operations interface component based on the aviation stability adjustment data and the aviation operations display data. As described above, in some embodiments, the stabilized aviation operations interface component includes one or more stabilized aviation operations display items corresponding to the aviation operations display items. For example, the stabilized aviation operations interface component can include one or more stabilized aviation operations display items including a flight plan display item, an altitude item, a speed display item, a heading display item, a remaining distance display item, an arrival time display item, a fuel consumption display item, an origin airport display item, a destination airport display item, a landing runway display item, a takeoff runway display item, a taxi display item, an aircraft type display item, etc.

[0111] In some embodiments, each of the one or more stabilized aviation operations display items is associated with a stabilized display item location on the stabilized aviation operations interface component. In this regard, for example, the stabilized display item location can be a location on the stabilized aviation operations interface component at which the stabilized aviation operations display item is displayed on and / or located on the stabilized aviation operations interface component. In some embodiments, the stabilized display item location can be a different location than the original display item location. In other words, in some embodiments, the stabilized aviation operations interface component is configured such that when displaying a display item associated with an aircraft operations item, an estimated change in position of an eye gaze of an operator of the aircraft (e.g., a pilot) and / or an estimated change in position of one or more of the airborne aviation stability equipment and / or one or more aircraft components due to an aviation instability event is considered.

[0112] In some embodiments, the stabilized aviation operations interface component includes one or more remapped touch zones. In some embodiments, the one or more remapped touch zones are selectable portions of the stabilized aviation operations interface component. For example, the one or more remapped touch zones can be selected to display information about a stabilized aviation operations display item of the one or more stabilized aviation operations display items. In some embodiments, the one or more remapped touch zones are associated with a remapped touch zone location on the stabilized aviation operations interface component. In this regard, for example, the remapped touch zone location can be a location on the stabilized aviation operations interface component at which a remapped touch zone of the one or more remapped touch zones is displayed on and / or located on the stabilized aviation operations interface component (e.g., touching the remapped touch zone location selects the remapped touch zone). In other words, for example, the one or more remapped touch zones can correspond to one or more touch zones but be located in different locations to address the aviation instability event.

[0113] As represented by block 510, the method 500 includes causing the stabilized aviation operation interface assembly to be presented to the aviation operation interface of the device. As described above, in some embodiments, the stabilized aviation operation interface assembly is disposed on the onboard aviation stabilization device and / or one or more of the one or more aircraft components. For example, the stabilized aviation operation interface assembly can be disposed on a multifunction control and display unit. In this regard, for example, the stabilized aviation operation interface assembly can be provided to an operator (e.g., a pilot) of the aircraft while the aircraft is performing an aviation mission.

[0114] As represented by optional block 512, the method 500 optionally includes identifying predicted aviation operation impact data. As described above, in some embodiments, the predicted aviation operation impact data includes one or more data items that represent and / or indicate a predicted aviation instability event. In this regard, in some embodiments, the predicted aviation instability event is a predicted event that is predicted to cause an acceleration motion (e.g., motion in the X-axis, Y-axis, and / or Z-axis) and / or an angular motion (e.g., azimuth motion, pitch motion, and / or roll motion) of the aircraft. Additionally or alternatively, the predicted aviation instability event is a predicted event that is predicted to cause an acceleration motion (e.g., motion in the X-axis, Y-axis, and / or Z-axis) and / or an angular motion (e.g., azimuth motion, pitch motion, and / or roll motion) of the onboard aviation stabilization device and / or one or more of the one or more aircraft components (e.g., an aircraft component on which the aviation operation interface is disposed). Additionally or alternatively, the predicted aviation instability event is a predicted event that is predicted to cause an acceleration motion (e.g., motion in the X-axis, Y-axis, and / or Z-axis) and / or an angular motion (e.g., azimuth motion, pitch motion, and / or roll motion) of an eye of an operator of the aircraft (e.g., an eye of a pilot).

[0115] In some embodiments, the predicted aviation instability event is a predicted takeoff associated with the aircraft. In this regard, for example, the predicted takeoff associated with the aircraft can be predicted to cause an acceleration motion (e.g., motion in the X-axis, Y-axis, and / or Z-axis) and / or an angular motion (e.g., azimuth motion, pitch motion, and / or roll motion) of the aircraft, the on-board aviation stabilization device, one or more aircraft components, and / or the eyes of an operator of the aircraft. In some embodiments, the predicted aviation instability event is a predicted landing associated with the aircraft. In this regard, for example, the predicted landing associated with the aircraft can be predicted to cause an acceleration motion (e.g., motion in the X-axis, Y-axis, and / or Z-axis) and / or an angular motion (e.g., azimuth motion, pitch motion, and / or roll motion) of the aircraft, the on-board aviation stabilization device, one or more aircraft components, and / or the eyes of an operator of the aircraft. In some embodiments, the predicted aviation instability event is a predicted weather associated with the aircraft. In this regard, for example, the predicted weather associated with the aircraft can be predicted to cause an acceleration motion (e.g., motion in the X-axis, Y-axis, and / or Z-axis) and / or an angular motion (e.g., azimuth motion, pitch motion, and / or roll motion) of the aircraft, the on-board aviation stabilization device, one or more aircraft components, and / or the eyes of an operator of the aircraft. In some embodiments, the predicted aviation instability event is a predicted turbulence associated with the aircraft. In this regard, for example, the predicted turbulence associated with the aircraft can be predicted to cause an acceleration motion (e.g., motion in the X-axis, Y-axis, and / or Z-axis) and / or an angular motion (e.g., azimuth motion, pitch motion, and / or roll motion) of the aircraft, the on-board aviation stabilization device, one or more aircraft components, and / or the eyes of an operator of the aircraft.

[0116] As shown in optional block 514, the method 500 optionally includes determining, based on the predicted aviation operation impact data, that the aircraft is predicted to be impacted by an aviation instability event. As described above, in some embodiments, the external aviation stabilization device and / or the on-board aviation stabilization device is configured to pre-generate aviation stability adjustment data such that, upon the aircraft being impacted by an aviation instability event, a stable aviation operation interface component can be presented. In this way, for example, the external aviation stabilization device and / or the on-board aviation stabilization device is able to provide a stable interface component (e.g., a stable aviation operation interface component) to an operator of the aircraft in a seamless manner.

[0117] Referring now to Figure 6 , a flowchart is shown that provides an example method 600. In this regard, Figure 6Operations that can be performed by the external aviation stability device 140, the aircraft 110, the one or more databases 170, the one or more aircraft components 130, and / or the onboard aviation stability device 180 are shown. In some embodiments, the method 600 includes operations for generating and / or causing to be presented an aviation operations interface component to an aviation operations interface, as described above. In some embodiments, the example method 600 defines a computer- implemented process that can be performed by any of the devices and / or systems embodied in hardware, software, firmware, and / or combinations thereof, as described herein. In some embodiments, computer program code comprising one or more computer code instructions is stored to at least one non-transitory computer-readable storage medium, such that execution of the computer program code initiates performance of the method 600.

[0118] As shown in block 602, the method 600 includes identifying aviation operation data. As described above, in some embodiments, the aviation operation data includes one or more data items that represent and / or indicate one or more aircraft operation items. In some embodiments, the aircraft operation item is an item associated with an aviation mission (e.g., an aviation mission performed by an aircraft). In this regard, in some embodiments, the aircraft operation item is a flight plan item. For example, the flight plan item can represent a flight plan that the aircraft is to follow to perform the aviation mission. In some embodiments, the aircraft operation item is an altitude item. For example, the altitude item can represent one or more altitudes at which the aircraft is to operate to perform the aviation mission. In some embodiments, the aircraft operation item is a speed item. For example, the speed item can represent one or more speeds at which the aircraft is to operate to perform the aviation mission.

[0119] In some embodiments, the aircraft operation item is a heading item. For example, the heading item can represent one or more headings that the aircraft is to follow to perform the aviation mission. In some embodiments, the aircraft operation item is a remaining distance item. For example, the remaining distance item can represent a distance that the aircraft still needs to travel to perform the aviation mission. In some embodiments, the aircraft operation item is an arrival time item. For example, the arrival time item can represent a time at which the aircraft is to arrive at a destination airport. In some embodiments, the aircraft operation item is a fuel consumption item. For example, the fuel consumption item can represent an amount of fuel that the aircraft has used while performing the aviation mission. In some embodiments, the aircraft operation item is an originating airport item. For example, the originating airport item can represent an airport from which the aircraft originated in the aviation mission.

[0120] In some embodiments, the aerial operation item is a destination airport item. For example, the destination airport item can represent an airport that the aircraft is traveling to in the aerial mission. In some embodiments, the aerial operation item is a landing runway item. For example, the landing runway item can represent a runway that the aircraft will land on in the aerial mission. In some embodiments, the aerial operation item is a takeoff runway item. For example, the takeoff runway item can represent a runway that the aircraft will take off from in the aerial mission. In some embodiments, the aerial operation item is a taxi item. For example, the taxi item can represent a taxi route that will be used by the aircraft for taxiing in the aerial mission. In some embodiments, the aerial operation item is an aircraft type item. For example, the aircraft type item can represent an aircraft type of the aircraft.

[0121] In some embodiments, identifying the aerial operation data includes the external aerial stabilization device and / or the onboard aerial stabilization device being configured to receive the aerial operation data. For example, the external aerial stabilization device and / or the onboard aerial stabilization device can be configured to receive the aerial operation data from an operator of the aircraft (e.g., a pilot). As another example, the external aerial stabilization device and / or the onboard aerial stabilization device can be configured to receive the aerial operation data from one or more databases. In some embodiments, identifying the aerial operation data includes the external aerial stabilization device and / or the onboard aerial stabilization device being configured to generate the aerial operation data. For example, the external aerial stabilization device and / or the onboard aerial stabilization device can be configured to generate the aerial operation data using one or more aircraft components.

[0122] As shown in block 604, the method 600 includes generating an aerial operation interface component based on the aerial operation data. As described above, in some embodiments, the aerial operation interface component includes one or more aerial operation display items configured to display one or more aerial operation items. For example, the aerial operation interface component can include one or more aerial operation display items including a flight plan display item, an altitude display item, a speed display item, a heading display item, a remaining distance display item, an arrival time display item, a fuel consumption display item, an origin airport display item, a destination airport display item, a landing runway display item, a takeoff runway display item, a taxi display item, an aircraft type display item, etc. In some embodiments, each of the one or more aerial operation display items is associated with an original display item location on the aerial operation interface component. In this regard, for example, the original display item location can be a location on the aerial operation interface component at which and / or where the aerial operation display item is displayed on and / or located on the aerial operation interface component.

[0123] In some embodiments, the aviation operating interface component includes one or more touch areas. In some embodiments, the one or more touch areas are optional portions of the aviation operating interface component. For example, the one or more touch areas may be selected to display information about one or more aviation operating display items. Additionally or alternatively, the one or more touch areas may be configured to control the aircraft and / or one or more components of the aircraft.

[0124] In some implementations, one or more touch areas are associated with an original touch area location on the aviation operating interface component. In this regard, for example, the original touch area location may be the location where one or more touch areas on the aviation operating interface component are displayed and / or located on the aviation operating interface component (e.g., touching the original touch area location selects the touch area).

[0125] As shown in box 606, method 600 includes presenting an aviation operation interface component on an aviation operation interface. As described above, in some embodiments, the aviation operation interface is located on one or more aircraft components, including airborne air stability equipment and / or one or more aircraft components. For example, the aviation operation interface may be located on a multifunction control and display unit. In this regard, for example, the aviation operation interface may be provided to the operator of the aircraft (e.g., a pilot) while the aircraft is performing an aviation mission.

[0126] The operations and / or functions of this disclosure have been described herein, such as in flowcharts. It should be understood that computer program instructions may be loaded onto a computer or other programmable device (e.g., hardware) to produce a machine, such that the resulting computer or other programmable device performs the operations and / or functions described in the flowchart frames herein. These computer program instructions may also be stored in a computer-readable storage medium that instructs a computer, processor, or other programmable device to operate and / or function in a particular manner, such that the instructions stored in the computer-readable storage medium produce an article of manufacture, the execution of which performs the operations and / or functions described in the flowchart frames. The computer program instructions may also be loaded onto a computer, processor, or other programmable device to cause a series of operations to be performed on the computer, processor, or other programmable device, thereby producing a computer-implemented process, such that the instructions, which execute on the computer, processor, or other programmable device, provide operations for implementing the functions and / or operations specified in the flowchart frames. Flowchart frames support combinations of components for performing the specified operations and / or functions, as well as combinations of operations and / or functions for performing the specified operations and / or functions. It should be understood that one or more boxes in a flowchart, as well as combinations of boxes in a flowchart, can be implemented by a hardware-based dedicated computer system or a combination of dedicated hardware and computer instructions that performs the specified operations and / or functions.

[0127] While the specification contains many specific implementation details, these should not be construed as limiting the scope of any disclosures or of what can be claimed, but as merely providing description of particular implementations. Certain features that are, for clarity, described above in the context of separate implementations can also be provided in combinations. Conversely, various features that are, for brevity, described above in the context of a single implementation can also be provided separately or in any suitable subcombination. In addition, while features can be described above as being implemented in certain combinations and even initially claimed as such, one or more features from a claimed combination can in some cases be excised from the combination and the claimed combination can be directed to a subcombination or variation of a subcombination.

[0128] While operations and / or functions are illustrated in the drawings in a particular, chronological order, this should not be understood as requiring such order unless specifically specified that an operation be performed or events occur in a particular order. One of ordinary skill in the art will also recognize that some operations can take different steps at different times or be performed in different orders than those described or otherwise illustrated herein, and that such embodiments are also contemplated. All such modifications and variations are within the skilled in the art's scope of the present disclosure.

[0129] Similarly, while operations are illustrated in the drawings in a particular order, this should not be understood as requiring such order unless specifically stated for that order. One of ordinary skill in the art will also recognize that some operations can take different steps at different times or be performed in different orders than those described or otherwise illustrated herein, and that such embodiments are also contemplated.

Claims

1. A method comprising: receiving aviation operation display data associated with an aircraft; capturing aviation operation impact data using one or more aircraft components of the aircraft, wherein the aviation operation impact data is indicative of an aviation instability event; generating aviation stability adjustment data by applying the aviation operation impact data to an aviation stability adjustment model; generating a stable aviation operation interface component based on the aviation stability adjustment data and the aviation operation display data, wherein the stable aviation operation interface component comprises one or more stable aviation operation display items; and causing the stable aviation operation interface component to be presented to an aviation operation interface of a device.

2. The method of claim 1, wherein the aviation operation interface comprises one or more touch zones.

3. The method of claim 1, wherein the stable aviation operation interface component comprises one or more remapped touch zones.

4. The method of claim 1, further comprising: identifying predicted aviation operation impact data; and determining that the aircraft is predicted to be affected by the aviation instability event based on the predicted aviation operation impact data.

5. The method of claim 1, further comprising: identifying aviation operation data; generating an aviation operation interface component based on the aviation operation data, wherein the aviation operation interface component comprises one or more aviation operation display items; and causing the aviation operation interface component to be presented on the aviation operation interface.

6. The method of claim 1, wherein the aviation instability event is one or more of a landing associated with the aircraft, a takeoff associated with the aircraft, weather associated with the aircraft, or turbulence associated with the aircraft.

7. The method of claim 1, wherein the aviation operation impact data is captured while the aircraft is performing an aviation mission.

8. The method of claim 1, wherein the device is a flight management system, an electronic flight bag, or a multifunction control and display unit.

9. An apparatus comprising a memory and one or more processors communicatively coupled to the memory, the one or more processors configured to: receive aviation operation display data associated with an aircraft; capture aviation operation impact data using one or more aircraft components of the aircraft, wherein the aviation operation impact data is indicative of an aviation instability event; generate aviation stability adjustment data by applying the aviation operation impact data to an aviation stability adjustment model; generate a stable aviation operation interface component based on the aviation stability adjustment data and the aviation operation display data, wherein the stable aviation operation interface component comprises one or more stable aviation operation display items; and cause the stable aviation operation interface component to be presented to an aviation operation interface of a device. ​ ​ 10. A computer program product, the computer program product comprising at least one non-transitory computer-readable storage medium having computer program code stored thereon, the computer program code, when executed by at least one processor, configuring the computer program product to: receive aerial operations display data associated with an aerial vehicle; capture aerial operations impact data using one or more aerial vehicle components of the aerial vehicle, wherein the aerial operations impact data is indicative of an aerial instability event; generate aerial stability adjustment data by applying the aerial operations impact data to an aerial stability adjustment model; generate a stable aerial operations interface component based on the aerial stability adjustment data and the aerial operations display data, wherein the stable aerial operations interface component comprises one or more stable aerial operations display items; and cause the stable aerial operations interface component to be presented to an aerial operations interface of a device.

Images