Control method and control device based on real-time dynamic state of aircraft

Abstract

The invention relates to a real-time dynamic control method and control device based on an aircraft, and the method comprises the following steps: obtaining a management mode, and if the management mode is a plan application mode, sequentially receiving plan application information, release application information, approach application information, take-off application information and landing application information, the received information is audited, and corresponding flight control is executed based on the audited information; if the management mode is a plan reporting mode, receiving plan reporting information, and performing synchronization processing on the plan reporting information passing the audit; wherein if the aircrafts can execute the flight plan or the landing plan according to the queuing sequence, the release application information or the landing application information passes auditing, and control over the take-off or landing process of the aircrafts is executed based on the dynamic information. Compared with the prior art, the method has the advantages of being more intelligent and automatic, improving the operation efficiency and the like.

Description

Technical Field

[0001] The present invention relates to the technical field of aircraft flight management and control, and particularly to a control method and a control device based on real-time dynamics of an aircraft. Background Art

[0002] The existing civil aviation closed-loop management process mainly relies on manual management supplemented by system support. This management mode can ensure flight safety under the complexity, safety and coordination requirements in civil aviation operation, but it also exposes multiple technical drawbacks and limitations:

[0003] 1. Manual-dominated and inefficient: In the closed-loop management of civil aviation, manual operations by tower controllers, dispatchers, etc. are the core, and the system only serves as an auxiliary tool. The manual management method is easily affected by factors such as the working pressure of controllers and human resource limitations, resulting in low approval and coordination efficiency. Especially during peak periods or in complex airspace situations, delays or poor scheduling are likely to occur.

[0004] 2. Heavy workload of controllers: In a complex airspace management and high-traffic flight environment, tower controllers need to continuously conduct a large amount of flight command and coordination, making it difficult to avoid fatigue and human errors. This management mode highly relies on personal experience and judgment, has operation bottlenecks, and cannot meet the requirements of more complex and denser airspace traffic management.

[0005] 3. Insufficient system reliance: Although there is partial system support for the process, the responsibilities and functions of the existing closed-loop management system are still relatively vague. The system is more for recording, monitoring and assisting rather than automatic decision-making or intelligent scheduling. This makes the management process highly dependent on manual decision-making and difficult to fully utilize technology to improve operation efficiency.

[0006] 4. Unable to meet the high-density flight demand: The existing management mode in the civil aviation field is applicable to relatively low-density flight activities in the medium and high altitude airspace. However, in the low-altitude scenario, there are more aircraft, higher takeoff / landing and navigation frequencies. The existing manual-based mode is obviously unable to cope with this high-density takeoff / landing and concurrent flight demand, and the human scheduling ability is also difficult to expand in a short time to handle the low-altitude area. With the increase in the number of low-altitude aircraft, the existing civil aviation closed-loop management mode is difficult to effectively expand to the low-altitude scenario.

[0007] The existing Chinese patent CN104332072B discloses a general aviation flight plan management system, including a flight plan database, a plan cycle management module, a plan generation and reporting module, a plan data service module, and a system operation module. It can quickly generate and share flight plans according to the real-time status of general aviation flights, and realizes the ability of general aviation users and control departments to complete the rapid establishment, reporting, approval, and management services of flight plans within the flight plan approval time limit and flight plan reporting time limit. However, this existing technology does not consider the closed-loop management in the low-altitude scenario and cannot meet the efficient requirements of each link. Summary of the Invention

[0008] The purpose of the present invention is to overcome the defects of the above-mentioned existing technology and provide a more intelligent and automated control method and control device based on the real-time dynamics of aircraft.

[0009] The purpose of the present invention can be achieved by the following technical solutions:

[0010] In the first aspect of the present invention, a control method based on the real-time dynamics of aircraft is provided, including the following steps:

[0011] S1) Obtain the management mode. If the management mode is the plan application mode, execute step S2; if the management mode is the plan reporting mode, execute step S3;

[0012] S2) Sequentially receive plan application information, release application information, approach application information, takeoff application information, and landing application information, review the received information, and perform corresponding flight control based on the information that passes the review;

[0013] S3) Receive plan reporting information and perform synchronization processing on the plan reporting information that passes the review;

[0014] Among them, in step S2, if the aircraft can execute the flight plan according to the queuing order, the release application information passes the review, and the takeoff process control of the aircraft is performed based on the dynamic information; if the aircraft can execute the landing plan according to the queuing order, the landing application information passes the review, and the landing process control of the aircraft is performed based on the dynamic information;

[0015] Among them, the dynamic information includes at least one or more of the real-time position and motion state of the aircraft, the dynamic state of ground personnel, the position and path of the tractor, and the real-time state of other aircraft on the airfield.

[0016] Furthermore, the plan application information is generated based on airspace information, and / or the plan reporting information is generated based on airspace information.

[0017] Further, the planned application information at least includes one or more of takeoff and landing point information, route information, mission information, aircraft model and ID, and time period information.

[0018] Further, the planned reporting information at least includes one or more of takeoff and landing point information, flight airspace information, aircraft model and ID, and time period information.

[0019] Further, the approved planned application information and the planned reporting information are both matched with a unique planned ID.

[0020] Further, when auditing the approach application information, it is implemented in combination with the unique planned ID.

[0021] Further, the process of determining that the release application information passes the audit includes:

[0022] Determine whether a special situation is detected.

[0023] If so, adjust and update the queuing order, and automatically approve the release application information according to the updated queuing order.

[0024] If not, directly approve the release application information automatically according to the current queuing order.

[0025] Further, the process of determining that the landing application information passes the audit includes:

[0026] Determine whether a special situation is detected.

[0027] If so, adjust and update the queuing order, and automatically approve the landing application information according to the updated queuing order.

[0028] If not, directly approve the landing application information automatically according to the current queuing order.

[0029] Further, the queuing order is automatically generated based on a predetermined time cycle.

[0030] Further, the adjustment and update of the queuing order are implemented based on a manual intervention instruction.

[0031] Further, the adjustment and update of the queuing order include:

[0032] The adjustment range is the release application information or the landing application information that has not passed the audit.

[0033] Further, the control of the takeoff or landing process specifically includes:

[0034] Judge whether there is a risk of conflict and collision according to the dynamic information. If so, output an avoidance instruction, where the avoidance instruction includes a braking instruction and / or a direction-changing instruction.

[0035] Furthermore, it further includes:

[0036] S4) Receive the departure report and conduct an audit.

[0037] In a second aspect of the present invention, there is provided a control device based on the real-time dynamics of an aircraft, including a logical operation unit, a storage device, and a ground-aircraft communication device. The logical operation unit is respectively signal-connected to the storage device and the ground-aircraft communication device. Among them,

[0038] The storage device is used to store all the aircraft parameter information to be run;

[0039] The ground-aircraft communication device is used to realize the communication between the control device and the ground or other aircraft;

[0040] Based on the stored data of the storage device and the communication data of the ground-aircraft communication device, the logical operation unit realizes the closed-loop management of the aircraft based on the control method based on the real-time dynamics of the aircraft as described above.

[0041] In a third aspect of the present invention, there is provided a control device based on the real-time dynamics of an aircraft, including an air traffic control terminal and an operator terminal, a ground crew terminal, and a drone pilot terminal respectively connected to the air traffic control terminal. Among them,

[0042] The operator terminal is used to send plan application information, takeoff application information, or plan reporting information;

[0043] The ground crew terminal is used to send approach application information;

[0044] The drone pilot terminal is used to send takeoff application information or landing application information;

[0045] Based on the control method based on the real-time dynamics of the aircraft as described above, the air traffic control terminal realizes the closed-loop management of the aircraft.

[0046] Compared with the prior art, the present invention has the following beneficial effects:

[0047] 1) The present invention fully intervenes in the decision-making and scheduling links, can automatically optimize the route and airspace resource allocation based on real-time data, reduces the dependence on manual intervention, and improves the operation efficiency.

[0048] 2) The present invention realizes the closed-loop management and control of aircraft operations, including flight plan management, route planning, conflict detection and resolution, etc., and can ensure that each management link is automatically or semi-automatically completed by the system, reducing the manual burden.

[0049] 3) In the low-altitude scenario, there are a large number of aircraft and a high flight density. The present invention completes dynamic scheduling and real-time instruction issuance through intelligent management, without relying solely on manual command, ensuring the response speed and efficiency.

[0050] 4) Based on strict operation specifications and procedures, the present invention ensures the standardization and controllability of operations in each link, ensuring that various flight activities can be carried out efficiently and safely within a unified framework.

[0051] 5) In the control device based on the real-time dynamics of the aircraft of the present invention, the issued instructions can be directly transmitted to the terminal device or the relevant person in charge, and the instructions can be executed in a timely manner, reducing delays or errors caused by intermediate transmission links.

[0052] 6) In the present invention, all data such as scheduling instructions, route planning, flight trajectories, etc. should be recorded to ensure the traceability of flight activities, facilitating subsequent review, analysis, and improvement. BRIEF DESCRIPTION OF THE DRAWINGS

[0053] Figure 1 is a schematic flow chart of the control method of the present invention;

[0054] Figure 2 is a schematic flow chart of the planned application mode of the present invention;

[0055] Figure 3 is a schematic diagram of the planned application judgment strategy of the present invention;

[0056] Figure 4 is a schematic diagram of the realization of the operation closed-loop management of each role in the planned application mode in the embodiment of the present invention;

[0057] Figure 5 is a schematic diagram of the management of each role during the takeoff stage in the embodiment of the present invention;

[0058] Figure 6 is a schematic diagram of the management of each role during the landing stage in the embodiment of the present invention;

[0059] Figure 7 is a schematic diagram of the aircraft takeoff and landing plan and the operation monitoring and avoidance process in the embodiment of the present invention;

[0060] Figure 8 is a schematic flow chart of the planned reporting mode of the present invention;

[0061] Figure 9 is a schematic diagram of the realization of the operation closed-loop management of each role in the planned reporting mode in the embodiment of the present invention;

[0062] Figure 10 is a schematic diagram of a control device based on the real-time dynamics of an aircraft provided in the embodiment of the present invention. DETAILED DESCRIPTION OF THE INVENTION

[0063] The present invention will be described in detail below with reference to the accompanying drawings and specific embodiments. This embodiment is implemented on the premise of the technical solution of the present invention, and provides a detailed implementation manner and a specific operation process. However, the protection scope of the present invention is not limited to the following embodiments.

[0064] Embodiment 1

[0065] With the increase in the number of low-altitude aircraft, the existing civil aviation closed-loop management mode is difficult to effectively expand to the low-altitude scenario. Therefore, in the low-altitude field, it is particularly necessary to develop a more intelligent and automated closed-loop operation management method and device. As Figure 1 shown, this embodiment provides a control method based on the real-time dynamics of aircraft. This method runs in the air traffic control system and includes the following steps:

[0066] S1) Obtain the management mode. If the management mode is the planned application mode, then execute step S2. If the management mode is the planned reporting mode, then execute step S3;

[0067] S2) Sequentially receive the planned application information, takeoff application information, approach application information, takeoff application information, and landing application information, review the received information, and perform corresponding flight control based on the information that passes the review, including takeoff or landing control, etc. Among them, when reviewing the takeoff application information or the landing application information, it is judged whether the review passes based on whether the aircraft can execute the flight plan or the landing plan in the queuing order, and the takeoff or landing process control of the aircraft is performed based on the dynamic information;

[0068] S3) Receive the planned reporting information and perform synchronization processing on the planned reporting information that passes the review.

[0069] The above method implements two strategies: the planned application mode and the planned reporting mode.

[0070] As Figure 2 , Figure 3 and Figure 4 shown, the planned application mode includes 6 stage processes: planned application, takeoff application, approach application, takeoff application, landing application, and departure notification, and realizes the operation closed-loop management in the planned application mode through the interaction of four roles: the air traffic control system, the operator, the ground crew, and the drone pilot. The air traffic control system has a planning desk workstation and a surveillance desk workstation, and is equipped with corresponding seat personnel. Specifically:

[0071] Step 101, planned application:

[0072] a. The operator logs in to the App;

[0073] b. The system synchronizes the airspace information (routes, airways) to the operator;

[0074] c. The operator submits a flight plan application, including the takeoff and landing points, route, mission, aircraft model and ID, time period, and pilot ID (not required);

[0075] d. The system receives the plan application information and conducts a review. If the review fails, the application is rejected and returned to step 101. The operator can choose to cancel or modify it and submit it again. If the review is passed, the system replies to the operator with the plan approval and the unique plan ID;

[0076] e. The operator modifies the pilot ID on the system;

[0077] f. The system replies with a modification receipt.

[0078] Step 102, Takeoff application:

[0079] a. The operator submits a takeoff application 1 hour in advance (configurable according to project requirements);

[0080] b. The system calculates whether the aircraft can execute the takeoff plan in the queuing order and conducts a takeoff review. At the same time, the seat personnel can manually confirm or change the queuing order in advance. If the review fails, the application is rejected and returned to step 102. The operator can choose to cancel or modify it and submit it again;

[0081] c. If the review is passed, the system replies with a receipt.

[0082] Step 103, Approach application:

[0083] a. The ground crew sends the approach application and the flight plan ID to the system;

[0084] b. The monitoring seat checks the plan. If the review fails, the application is rejected and returned to step 103. The ground crew can choose to cancel or modify it and submit it again, and the review result is feedback to the ground crew (allowed / not allowed);

[0085] c. The ground crew sends the approach notice to the system;

[0086] d. The system replies to the ground crew that the approach confirmation has been received.

[0087] Step 104, Takeoff request:

[0088] a. The pilot logs in to the system (App);

[0089] b. The system synchronizes the approved flight plan to the pilot's terminal;

[0090] c. The pilot sends a takeoff request to the system;

[0091] d. If the review by the monitoring seat of the system fails, the application is rejected and returned to step 104. The pilot can choose to cancel or modify it and submit it again;

[0092] e. If the review at the monitoring station is passed, the system sends a consent receipt with a time window (e.g., the validity period is 3 minutes) to the drone operator.

[0093] f. If the ground crew's review is not passed, the application is rejected and returned to step 104. The drone operator can choose to cancel or modify and resubmit.

[0094] g. If the ground crew's review is passed, a consent receipt (the monitoring station agrees, the ground crew agrees, and within the time window) is sent to the drone operator.

[0095] h. The ground crew sends a report of having taken off to the system (monitoring station).

[0096] The above process of takeoff application, review, and execution of the takeoff application is as Figure 5 shown.

[0097] Step 105, landing application:

[0098] a. The drone operator sends a landing application to the system.

[0099] b. The system calculates whether the aircraft can execute the landing plan according to the queuing order. The seat personnel can manually confirm or change the queuing order in advance.

[0100] c. If the review at the monitoring station of the system is not passed, the application is rejected and returned to step 105. The drone operator can choose to cancel or modify and resubmit.

[0101] d. If the review at the monitoring station is passed, the system sends a consent receipt to the drone operator.

[0102] e. If the ground crew's review is not passed, the application is rejected and returned to step 105. The drone operator can choose to cancel or modify and resubmit.

[0103] f. If the ground crew's review is passed, a consent receipt is sent to the drone operator.

[0104] g. The ground crew sends a report of having landed to the system (monitoring station).

[0105] The above process of landing application, review, and execution of the takeoff application is as Figure 6 shown.

[0106] Step 106, departure notice:

[0107] a. The ground crew sends a departure report to the system.

[0108] b. The system gives a feedback receipt to the ground crew.

[0109] When reviewing the takeoff application information or landing application information, it is judged whether the review is passed based on whether the aircraft can execute the flight plan or landing plan according to the queuing order, and it is judged whether a special situation is detected. If so, the queuing order is adjusted and updated, and the takeoff application information or landing application information is automatically approved according to the updated queuing order. If not, the takeoff application information or landing application information is directly approved automatically according to the current queuing order. Taking the execution of the flight plan as an example, as Figure 7 shows the whole process of plan review and dynamic management. By integrating the automated management of flight plans and dynamic conflict monitoring, the safety and efficiency of aircraft operations on the ground and in the air can be ensured, as described in detail below:

[0110] Step 201, Submitting the flight plan for approval:

[0111] The flight plan is submitted to the air traffic control system based on the scheduled time and airspace requirements.

[0112] Step 202, Automatic queuing:

[0113] a. The system automatically queues the flight plans according to the scheduled time;

[0114] b. For flight plans without special situations, the system issues takeoff confirmations in sequence according to the queuing order.

[0115] Step 203, Judging special situations:

[0116] Judge whether there are special situations. If so, trigger the special situation handling and go to Step 204. If not, go to Step 206. In this embodiment, the judgment conditions for special situations can be configured according to the actual situation.

[0117] Step 204, Triggering special situations:

[0118] Trigger the condition for manual intervention and change the queuing order.

[0119] Step 205, Manual intervention:

[0120] a. The personnel in the planned seat enter the queuing list management interface;

[0121] b. Manual intervention operation: Use the mouse to click and drag to select the flight plan to adjust the queuing order.

[0122] c. After manual adjustment, the air traffic control system updates the queuing list;

[0123] d. The updated plan order issues takeoff confirmations automatically according to the new order.

[0124] When changing the queuing order, the allowable adjustment range is only for flight plans for which release confirmation has not been sent. Flight plans for which release confirmation has been sent cannot be adjusted and need to wait until they are executed.

[0125] Step 206, automatically send release confirmation:

[0126] a. The system automatically sends release confirmation in the air traffic control system. After the sending is completed, the status of this flight plan changes to "release confirmed".

[0127] b. Plans that have been confirmed for release cannot be manually adjusted.

[0128] The system continuously monitors whether new flight plans are submitted and processes them according to the automatic queuing rules. Flight plans that need to be changed will trigger manual intervention and adjustment under special circumstances.

[0129] Step 207, aircraft movement on the apron:

[0130] The aircraft starts to move from the parking bay to the takeoff and landing area and prepares for takeoff.

[0131] Step 208, real-time dynamic reception and monitoring:

[0132] The system receives the following dynamic information in real time:

[0133] ● The real-time position and movement status of the aircraft;

[0134] ● The dynamics of ground personnel;

[0135] ● The position and path of the tractor;

[0136] ● The real-time status of other aircraft on the apron.

[0137] Step 209, conflict and collision risk monitoring:

[0138] The system determines whether there are the following risks through dynamic data analysis:

[0139] ● Ground path conflicts.

[0140] ● In-air flight route conflicts.

[0141] ● Potential collision risks.

[0142] If so, execute Step 210; otherwise, execute Step 211.

[0143] Step 210, risk decision-making and instruction output:

[0144] If the system detects risks:

[0145] ● Adjust the ground and in-air flight routes of the aircraft according to the real-time data.

[0146] ● Output avoidance instructions, such as:

[0147] ○ Braking instruction: Require the aircraft to decelerate or stop.

[0148] ○ Course change instruction: Change the ground travel path or the air route.

[0149] Step 211, continuous dynamic monitoring

[0150] The system continuously and real-time monitors the dynamics before and after the aircraft takes off, and repeatedly executes risk judgment and instruction adjustment until the aircraft completes ground operation, takes off safely, or completes air operation.

[0151] As Figure 8 and Figure 9 shown, the specific process of the planned filing mode in this embodiment includes:

[0152] Step 301, planned filing:

[0153] a. The operator logs in to the App;

[0154] b. The system synchronizes airspace information (routes, airways) to the operator;

[0155] c. The operator submits a flight plan filing, including takeoff and landing points, flight airspace, aircraft model and ID, time period, and pilot ID (not required);

[0156] Step 302, filing synchronization:

[0157] a. The system replies to the operator with the plan approval and the unique ID of the plan;

[0158] b. If the review is passed, the system synchronizes the filed plan to the ground crew.

[0159] The above method can automatically optimize the route and airspace resource allocation based on real-time data, reduce the dependence on manual intervention, improve the operation efficiency, ensure that each management link is automatically or semi-automatically completed by the system, and reduce the manual burden by successively receiving plan application information, takeoff application information, approach application information, takeoff application information, and landing application information, reviewing the received information, and performing corresponding takeoff or landing control based on the information passed the review.

[0160] Embodiment 2

[0161] This embodiment provides a control device based on the real-time dynamics of an aircraft, as Figure 10As shown in the figure, it includes a logical operation unit 1, a storage device 2, and a ground-aircraft communication device 3. The logical operation unit 1 is respectively signal-connected to the storage device 2 and the ground-aircraft communication device 3. Among them, the storage device 2 is used to store all possible aircraft parameter information that can operate; the ground and aircraft communication device 3 is used to realize the communication between the control device and the ground or other aircraft; the logical operation unit 1 realizes the closed-loop management of the aircraft based on the control method based on the real-time dynamics of the aircraft as described in Embodiment 1 according to the stored data of the storage device and the communication data of the ground and aircraft communication device.

[0162] In this embodiment, the logical operation unit can obtain the current position, speed, and planned queuing order of the aircraft, and calculate whether the aircraft can execute the takeoff and landing plans according to the queuing order based on the information of ground personnel, tractors, and other aircraft obtained from the ground and aircraft communication device, as well as the electronic map and all possible aircraft parameter information on the airfield obtained from the storage device. It also calculates whether there is a risk of collision for the aircraft and determines whether to change the operation route or output an emergency brake.

[0163] Embodiment 3

[0164] This embodiment provides a control device based on the real-time dynamics of the aircraft, including an air traffic control terminal and an operator terminal, a ground crew terminal, and a drone pilot terminal respectively connected to the air traffic control terminal. Among them, the operator terminal is used to send plan application information, flight release application information, or plan reporting information; the ground crew terminal is used to send approach application information; the drone pilot terminal is used to send takeoff application information or landing application information; the air traffic control terminal realizes the closed-loop management of the aircraft based on the control method based on the real-time dynamics of the aircraft as described in Embodiment 1.

[0165] The above terminals respectively correspond to the four roles of the air traffic control system, the operator, the ground crew, and the drone pilot. Based on the interaction of the four roles, the closed-loop operation management of the plan application strategy is carried out in stages. Among them, the air traffic control system has a plan desk workstation and a surveillance desk workstation, and is equipped with corresponding seat personnel. Through the surveillance desk interface, the drone pilot terminal APP interface, the ground crew terminal APP interface, and the operator terminal APP interface, the full coverage of the monitoring station-node-terminal is completed. It has 6-stage processes such as plan application (plan desk), flight release application (surveillance desk), approach application (surveillance desk), takeoff application (surveillance desk), landing application (surveillance desk), and departure notice (surveillance desk), forming a plan application strategy closed-loop process composed of key internal states such as flight plan application submission, flight application approval, flight release application submission, flight release application approval, approach application submission, surveillance desk allowing approach, approach notice, takeoff application, monitoring desk allowing takeoff, ground crew allowing takeoff, takeoff report, landing application, monitoring desk allowing landing, ground crew allowing landing, landing report, and departure report.

[0166] The above control device based on the real-time dynamics of the aircraft can simultaneously implement the closed-loop management of the plan reporting strategy that is only applicable to light and small aircraft. It only manages the reporting of plans, without the need to submit specific flight routes or select the existing air traffic routes in the system. It can fly freely in a closed airspace, with relatively high freedom and strong operability. The order and safety of approach, takeoff, landing, and departure are the responsibilities of the pilot and ground crew, and the system has low safety risks.

[0167] In other embodiments, an electronic device applicable to the plan application strategy and the plan reporting strategy may be provided, including a memory and a processor. A computer program is stored on the memory, and when the processor executes the program, the above method is implemented.

[0168] In other embodiments, a computer-readable storage medium applicable to the plan application strategy and the plan reporting strategy may be provided, on which a computer program is stored. When the program is executed by a processor, the above method is implemented.

[0169] The electronic device of the present invention includes a central processing unit (CPU), which can execute various appropriate actions and processes according to the computer program instructions stored in the read-only memory (ROM) or the computer program instructions loaded from the storage unit into the random access memory (RAM). In the RAM, various programs and data required for device operation can also be stored. The CPU, ROM, and RAM are connected to each other through a bus. The input / output (I / O) interface is also connected to the bus.

[0170] Multiple components in the device are connected to the I / O interface, including: an input unit, such as a keyboard, a mouse, etc.; an output unit, such as various types of displays, speakers, etc.; a storage unit, such as a disk, an optical disc, etc.; and a communication unit, such as a network card, a modem, a wireless communication transceiver, etc. The communication unit allows the device to exchange information / data with other devices through a computer network such as the Internet and / or various telecommunication networks.

[0171] The processing unit executes the various methods and processes described above. For example, in some embodiments, Figures 1 to 9 the methods described can be implemented as a computer software program, which is tangibly contained in a machine-readable medium, such as a storage unit. In some embodiments, part or all of the computer program can be loaded or installed onto the device via the ROM and / or the communication unit. When the computer program is loaded into the RAM and executed by the CPU, one or more steps described can be executed Figures 1 to 9 Alternatively, in other embodiments, the CPU can be configured to execute Figures 1 to 9 the methods and steps described in any other appropriate manner (for example, by means of firmware).

[0172] The functions described above in the present invention can be performed, at least in part, by one or more hardware logic components. For example, without limitation, exemplary types of hardware logic components that may be used include: Field Programmable Gate Arrays (FPGA), Application Specific Integrated Circuits (ASIC), Application Specific Standard Products (ASSP), System on a Chip (SOC), Complex Programmable Logic Devices (CPLD), and the like.

[0173] The program code for implementing the method of the present invention can be written in any combination of one or more programming languages. These program codes can be provided to a processor or controller of a general purpose computer, a special purpose computer, or other programmable data processing device, such that when the program codes are executed by the processor or controller, the functions / operations specified in the flowchart and / or block diagram are implemented. The program code can be executed entirely on the machine, partially on the machine, executed partially on the machine as an independent software package and partially on a remote machine, or executed entirely on a remote machine or server.

[0174] In the context of the present invention, a machine-readable medium can be a tangible medium that can contain or store a program for use by or in connection with an instruction execution system, apparatus, or device. A machine-readable medium can be a machine-readable signal medium or a machine-readable storage medium. A machine-readable medium can include, but is not limited to, electronic, magnetic, optical, electromagnetic, infrared, or semiconductor systems, apparatus, or devices, or any suitable combination of the foregoing. More specific examples of a machine-readable storage medium would include an electrical connection based on one or more wires, a portable computer diskette, a hard disk, a Random Access Memory (RAM), a Read-Only Memory (ROM), an Erasable Programmable Read-Only Memory (EPROM or Flash Memory), an optical fiber, a portable Compact Disc Read-Only Memory (CD-ROM), an optical storage device, a magnetic storage device, or any suitable combination of the foregoing.

[0175] The preferred specific embodiments of the present invention have been described in detail above. It should be understood that those of ordinary skill in the art can make many modifications and variations based on the concept of the present invention without creative efforts. Therefore, all technical solutions that can be obtained by those skilled in the art in the technical field of the present invention through logical analysis, reasoning, or limited experiments based on the concept of the present invention on the basis of the prior art should fall within the protection scope determined by the claims.

Claims

1. A control method based on real-time dynamics of an aircraft, characterized in that: The following steps are involved: S1) obtaining a management mode, if the management mode is a plan application mode, executing step S2, if the management mode is a plan reporting mode, executing step S3; S2) receiving the plan application information, the launch application information, the approach application information, the take-off application information and the landing application information in sequence, reviewing the received information, and executing corresponding flight control based on the reviewed information; S3) receiving plan filing information and synchronously processing the approved plan filing information; Wherein, in step S2, if the aircraft can execute the flight plan in the queue order, the release application information is reviewed, and the take-off process control of the aircraft is executed based on the dynamic information; if the aircraft can execute the landing plan in the queue order, the landing application information is reviewed, and the landing process control of the aircraft is executed based on the dynamic information; The dynamic information includes at least one or more of the real-time position and movement status of the aircraft, the dynamics of ground personnel, the position and path of the tractor, and the real-time status of other aircraft on the scene.

2. The control method based on real-time dynamics of an aircraft according to claim 1, characterized in that: The plan application information is generated based on airspace information, and / or the plan reporting information is generated based on airspace information.

3. The control method based on real-time dynamics of an aircraft according to claim 1, characterized in that: The plan application information includes at least one or more of take-off and landing point information, route information, mission information, aircraft model and ID, and time period information.

4. The control method based on real-time dynamics of an aircraft according to claim 1, characterized in that: The plan reporting information includes at least one or more of take-off and landing point information, flight airspace information, aircraft model and ID, and time period information.

5. The control method based on real-time dynamics of an aircraft according to claim 1, characterized in that: The approved plan application information and plan filing information are matched with the plan's unique ID.

6. The control method based on real-time dynamics of an aircraft according to claim 5, characterized in that: When reviewing the entry application information, it is implemented in combination with the unique ID of the plan.

7. The control method based on real-time dynamics of an aircraft according to claim 1, characterized in that: The process of determining whether the release application information has passed the review includes: Determine whether a special situation has been detected. If yes, the update queue order is adjusted, and the release application information is automatically approved according to the updated queue order. If not, the release application information will be automatically reviewed and approved according to the current queue order.

8. The control method based on real-time dynamics of an aircraft according to claim 1, characterized in that: The process of determining whether the landing application information has passed the review includes: Determine whether a special situation has been detected. If yes, the update queue order is adjusted, and the landing application information is automatically approved according to the updated queue order. If not, the landing application information will be automatically approved according to the current queue order.

9. The control method based on real-time dynamics of an aircraft according to claim 1, 7 or 8, characterized in that: The queue order is automatically generated based on a predetermined time cycle.

10. The control method based on real-time dynamics of an aircraft according to claim 7 or 8, characterized in that: The adjustment and updating of the queue order is implemented based on a manual intervention instruction.

11. The control method based on real-time dynamics of an aircraft according to claim 7 or 8, characterized in that: The adjusting and updating queueing sequence comprises: The adjustment scope includes the launch application information or landing application information that has not been reviewed and approved.

12. The control method based on real-time dynamics of an aircraft according to claim 1, characterized in that: The take-off or landing process control specifically includes: Determine whether there is a conflict and collision risk based on the dynamic information, and if so, output an avoidance instruction, wherein the avoidance instruction includes a braking instruction and / or a change of direction instruction.

13. The control method based on real-time dynamics of an aircraft according to claim 1, characterized in that: Also includes: S4) Receive and review the departure report.

14. A control device based on real-time dynamics of an aircraft, characterized in that: It includes a logic operation unit, a storage device, and a ground-aircraft communication device, wherein the logic operation unit is signal-connected to the storage device and the ground-aircraft communication device, respectively, wherein: The storage device is used to store all aircraft parameter information to be operated; The ground-to-aircraft communication equipment is used to realize the communication between the control device and the ground or other aircraft; The logic operation unit implements closed-loop management of the aircraft based on the control method based on real-time dynamics of the aircraft as described in any one of claims 1-13 according to the storage data of the storage device and the communication data of the ground and aircraft communication devices.

15. A control device based on real-time dynamics of an aircraft, characterized in that: It includes an air traffic control terminal and an operator terminal, a ground handling terminal and a pilot terminal respectively connected to the air traffic control terminal, wherein: The operator terminal is used to send plan application information, flight release application information or plan filing information; The ground handling terminal is used to send the approach application information; The pilot terminal is used to send take-off application information or landing application information; The air traffic control terminal realizes closed-loop management of the aircraft based on the real-time dynamic control method of the aircraft as described in any one of claims 1-13.

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