54 results about "Flight experience" patented technology

The invention relates to the technical field of unmanned aerial vehicle autonomous navigation, and discloses a mine unmanned aerial vehicle autonomous route dynamic adjustment system which comprises a multi-mode sensing module, a dynamic environment field potential modeling module, a field potential spatio-temporal evolution prediction module, a route wave function resolving and generating module, an unmanned aerial vehicle platform and flight control module and a self-adaptive calibration module. A safe and smooth air route expected position is generated in a predicted risk potential field by solving an air route wave function equation, and the core of the method is that a self-adaptive calibration module carries out closed-loop feedback adjustment on fusion weight of environment field potential by quantifying trajectory tracking deviation and flight stability deviation of actual flight of an unmanned aerial vehicle. According to the method, the problem that the risk model is solidified and cannot adapt to the dynamic environment in the prior art is solved, so that the unmanned aerial vehicle can autonomously learn and correct the cognition of the unmanned aerial vehicle on the environmental risk according to the actual flight experience, and the autonomous navigation adaptability and safety in the complex dynamic environment are remarkably improved.

The present invention provides a passenger seat allocation method and device, the method comprising: obtaining flight information, passenger information of each passenger and passenger flight segment information; dividing each passenger into an ordinary passenger group and a special passenger group according to the passenger information; setting a grouping priority corresponding to the special passenger group, and executing a seat allocation process corresponding to the special passenger group based on the grouping priority; the seat allocation process comprises: obtaining a seat map based on passenger flight segment information and flight information; determining the riding needs of special passengers; dividing each seat area in the seat map; based on the number of passengers corresponding to the special passenger group, screening out a target seat area, and allocating passengers in the special passenger group to each seat in the target seat area; after completing the seat allocation of all special passenger groups, allocating each ordinary passenger in each ordinary passenger group to an empty seat. Applying the method provided by the present invention, seats can be allocated in advance for special passengers and their accompanying personnel, thereby improving the passenger's flight experience.

The utility model discloses disposable aviation tableware, and relates to the field of disposable tableware, the disposable aviation tableware comprises a dinner plate, two sides of the dinner plate are provided with supporting handles, the dinner plate is internally provided with a supporting pipe, the upper end of the supporting pipe is provided with a clamping groove, and the lower ends of the dinner plate and the supporting pipe are provided with protruding points. A clamping strip ring is arranged at the upper end of the dinner plate, a dinner cover is arranged at the upper end of the dinner plate, a sealing edge is arranged at the side end of the dinner cover, and the dinner plate and the dinner cover are both made of full corn starch. Through the arrangement of the protruding points, the friction force between the dinner plate and the small table plate can be increased, the dinner plate can be effectively prevented from sliding due to jolting in the flying process, accidents such as food spilling or scalding can be avoided, the dining safety of passengers is guaranteed, the passengers can be more relieved during dining, and the service life of the dinner plate is prolonged. Through the detailed consideration, the flight experience of passengers can be improved, and the passengers can feel more comfortable and convenient.

The invention discloses a flight simulation training auxiliary system and method based on intelligent co-pilot, and the system comprises a data collection module which is used for collecting flight data and carrying out the operation monitoring of a college; the voice interaction interface is used for multi-mode state analysis voice interaction; the student model module is used for skill level evaluation and learning style identification; the emotion perception module is used for flight experience identification and risk prediction analysis; the personalized training module is used for training process monitoring, training result analysis and personalized training adjustment; and the decision engine module is used for deeply reinforcing a learning model and assisting a strategy generator. And intelligent and personalized auxiliary support is provided for pilot training. Through real-time data analysis and an adaptive learning algorithm, functions and behaviors of a real copilot are simulated, and targeted guidance is provided for flight trainees. And a complete training ecosystem is formed. And the flexibility and expandability of the system are ensured, and each functional component can be independently optimized and upgraded.

The invention provides a method and device for determining estimated arrival time, a medium and equipment, and relates to the technical field of data processing, and the method comprises the steps: obtaining a position coordinate information list Z of a target aircraft once every a first preset time period in response to the condition that the distance between the target aircraft and an airport to be landed is smaller than a preset distance; inputting the Z into a trajectory judgment model to obtain a target preset trajectory corresponding to the target aircraft; and according to the target preset track, the predicted arrival time of the target aircraft is updated every second preset time period. According to the invention, the predicted arrival time obtained by the target aircraft in the descent stage is more accurate, the accuracy of flight data prediction is improved, and the flight experience of a user is improved.

1. The name of the design product: VR back-mounted flight experience cockpit. 2. The use of the design product: This product is an entertainment device for providing virtual reality (VR) flight experience. Through the back-mounted design, users can feel the immersion during the experience. 3. The design key points of the design product: lies in the shape. 4. The picture or photo that best shows the design key points: the three-dimensional view.

The invention provides a mooring type manned amusement aircraft based on aerodynamic force and a using method thereof, and relates to the technical field of amusement equipment, the mooring type manned amusement aircraft comprises an aircraft body provided with a manned cabin, and an undercarriage is connected to the lower portion of the aircraft body; the power system comprises a plurality of electric rotor devices which are arranged on the aircraft body and are used for providing lift force; one end of the mooring cable assembly is connected with the machine body, and the other end of the mooring cable assembly is connected to a ground base station; the mooring cable assembly comprises a power line used for supplying power to the electric rotor wing device. And the flight control system is arranged in the aircraft body and / or the ground base station, is electrically connected with the electric rotor devices, and is used for controlling the aircraft to lift off, hover and recover. Low-cost and high-frequency operation is achieved through ground power supply, real immersive flexible flight experience can be provided, multiple safety protection is achieved, and safe and reliable operation under various sites is ensured.

The invention discloses a safety system for low-altitude wing-mounted flight and an operation method, the safety system comprises a first steel cable, a swinging rope, a whole-body safety belt and a diving platform, the diving platform is used for being installed on a first supporting structure, the diving platform is used for allowing a user to stand and take off, and the first steel cable extends in the horizontal direction; the two ends of the first steel cable are used for being connected to first steel rings on the two opposite sides of the second supporting structure respectively, the first end of the swinging rope is detachably connected to a first connecting point on the first steel cable, and a whole-body safety belt is arranged at the second end of the swinging rope and can be worn on the trunk part of a user located on the diving platform. Therefore, after a user jumps out of the diving platform, the swinging rope can be driven to do pendulum swinging motion in a vertical plane around the first connecting point. According to the safety system, the pendulum principle is utilized, traditional high-altitude protection equipment is combined, a wing-mounted flight experience mode which is stimulated and relatively safe is provided, and therefore the high threshold needed by traditional wing-mounted flight is lowered, and the technical requirements of traditional wing-mounted flight are lowered.

1. The name of this design product: UAV flight experience cabin (airport cantilevered side-mounted). 2. Purpose of this design product: for gaming and entertainment. 3. The design key point of this appearance design product lies in the shape. 4. The picture or photo that best illustrates the key points of the design: 3D drawing of Design 1. 5. Designate Design 1 as the base design.

The invention relates to an outdoor test flight verification platform for an intelligent fault-tolerant flight control system of a fixed-wing unmanned aerial vehicle, which relates to the field of unmanned aerial vehicles and is divided into an unmanned aerial vehicle platform and a ground platform. The unmanned aerial vehicle platform comprises a fixed-wing unmanned aerial vehicle model which is used for carrying equipment required by flight; the flight control board is used for measuring state information of the unmanned aerial vehicle and controlling flight; the airborne industrial personal computer is used for carrying a control algorithm and calculating and outputting a fault-tolerant control law to the flight control board; and the airborne data radio is used for communication between the unmanned aerial vehicle and the ground. The ground platform comprises a ground data radio station used for communication between the unmanned aerial vehicle and the ground; the Mission Planner ground station is used for displaying the state information and flight adjustment parameters of the unmanned aerial vehicle; and the fault-tolerant ground station is used for displaying a control algorithm output result and algorithm parameter adjustment. The outdoor test flight verification platform for the unmanned aerial vehicle can visually display the flight state of the unmanned aerial vehicle in the actual environment when the unmanned aerial vehicle breaks down, the test flight experience is accumulated, and the test flight trial and error cost is reduced.

The present invention relates to the technical field of unmanned aerial vehicles, and specifically to an unmanned aerial vehicle aileron structure and an unmanned aerial vehicle, comprising an unmanned aerial vehicle main body, a flight-assisting mechanism being provided at the front end of the unmanned aerial vehicle main body, and a main wing being installed above the unmanned aerial vehicle main body through a connecting assembly, and aileron mechanisms being provided at two locations on the upper ends of the main wing. The aileron structure of the unmanned fixed-wing aircraft can be expanded to increase the contact area with the wind during flight, so that a stronger reaction force can be provided when the wind becomes stronger, and the wind disturbance can be resisted. Furthermore, when flying in windy weather, the steering of the unmanned fixed-wing aircraft will be more sensitive, thereby improving the flight experience. The upper gap between the aileron structure and the main wing, where foreign objects are easily stuck, is shielded by a rubber bag, and the rubber bag will also shrink as the aileron structure rotates upward, and will be stretched and deformed as the aileron structure rotates downward, and will not affect the rotation of the aileron structure.

The utility model discloses a flight driving simulation game seat which comprises a base, a seat body and a handle are arranged on the base, a linkage plate is connected between the seat body and the handle, the lower end of the handle is connected with a transmission structure, a movable hole allowing the handle to penetrate through is formed in the linkage plate, and the linkage plate is connected with the transmission structure. The handle is pulled forwards and backwards to drive the transmission structure to move forwards and backwards in the base, or the handle is shifted leftwards and rightwards to link the linkage plate to drive the base body to swing leftwards and rightwards relative to the base. According to the game seat, when a user toggles the handle forwards and backwards, the mode that an airplane flies forwards and backwards can be simulated, when the handle is toggled leftwards and rightwards, the airplane flies leftwards or rightwards, meanwhile, the seat body can be driven to swing, and the flight experience feeling is enhanced.

The utility model provides a linkage tracking device which comprises a fixed stand column, driving assemblies, a carrying cable and a cable-embracing winch connecting assembly, the driving assemblies are respectively fixed on the fixed stand column, each driving assembly comprises a motor and a driving wheel, two ends of the carrying cable are respectively arranged on the driving wheels, and the motor provides power for the driving wheels so as to drive the carrying cable to move. The rope clip winch connecting assembly comprises a rope clip, a hook and an electric winch assembly, the rope clip is located on the carrying rope and moves along with the carrying rope, and the upper end of the hook is rigidly connected with the rope clip; the utility model further provides a flight experience system, the flight experience system comprises a linkage tracking device, a cable and an aircraft, the length of the cable ensures that the aircraft does not make contact with the ground in the cable full-release state, and the cable moves along with the aircraft and conducts automatic induction take-up and pay-off through the electric capstan. A guarantee with an extremely high safety coefficient can be provided for the aircraft, and the safety guarantee problem and the application scene problem of the aircraft in flight are effectively solved.

The invention discloses winch suspension type experience manned flight amusement equipment, belongs to the field of amusement equipment, and aims at solving the problems that existing equipment is short in endurance and poor in safety. The equipment comprises a winch system, a traction rope, an unmanned aerial vehicle and a power supply, the winch system comprises a winch frame, a pulley and an electric winch; a tension sensor is arranged at the electric winch or a traction rope; the unmanned aerial vehicle comprises a body and an experience cabin, and the experience cabin is provided with an intercom device and an infrared distance sensor; the power source supplies power to the electric winch and the unmanned aerial vehicle through power lines. The pulling force sensor can monitor pulling force of the pulling rope, and the electric winch is automatically locked and unwound when the unmanned aerial vehicle breaks down; and the infrared distance sensor can trigger locking of the traction rope during landing. The equipment is stable in endurance, high in safety and capable of providing safe flight experience for experiencers for a long time.

An unmanned aerial vehicle (UAV) includes: a body including a nose and a tail opposite to the nose; a plurality of rotor devices respectively mounted on the body; and a rear obstacle avoidance sensor mounted on a top part of the body, the UAV has a backward flight state of flying in a direction towards the tail and a hover state of stably hovering in a wind-free environment; in the hover state, the body is tilted in a length direction relative to a horizontal direction, so that the nose is higher than the tail; the optical axis of the rear obstacle avoidance sensor is tilted at a greater angle relative to the horizontal direction when the UAV is in the hover state compared to the backward flight state. It can improve the flight efficiency, enhance the overall obstacle avoidance function, and improve the flight experience.

The utility model relates to a manned aircraft flight experience system, which comprises more than two supports, a bearing cable, a power supply module, a tracking hanging module and an aircraft, the bearing cable is connected with two adjacent supports, the power supply module provides electric energy for the manned aircraft flight experience system, and the tracking hanging module is connected with the aircraft through a cable. The tracking and hanging module comprises a cable winding and unwinding device and a tracking device, the cable winding and unwinding device is used for automatically winding and unwinding a cable, the tracking device is rigidly connected with the cable winding and unwinding device, and the tracking device moves on the bearing cable along with the aircraft and tracks operation of the aircraft; through the accurate tracking and following technology of the cable take-up and pay-off device and the tracking device, it is guaranteed that the aircraft cannot be pulled, the flight safety is remarkably improved, the unmanned aerial vehicle can be applied to amusement places in the field of commercial operation, flight experience activities are provided, and the safety guarantee problem and the application scene problem of the unmanned aerial vehicle in the flight process are effectively solved.

1. The name of this design product: simulated cabin (without outer shell). 2. Purpose of this design product: used to simulate a flight cabin and provide a more open and immersive flight experience. 3. The design key point of this appearance design product lies in the shape. 4. The picture or photo that best illustrates the design points: three-dimensional picture.

The invention discloses a system and a method for pre-generating a civil aviation electronic boarding pass, and a medium. The system comprises a passenger information module used for storing detail data of all passengers in a flight to be executed; the check-in invitation module is used for determining passengers who do not select seats before a preset moment and sending check-in invitation information; the all seat dispatching module is used for periodically determining passengers to be dispatched in a flight to be executed after a preset moment and automatically dispatching seats; the automatic check-in module is used for automatically handling check-in for the passengers who have selected seats or dispatched seats and meet the online check-in condition; the electronic boarding check module is used for providing electronic boarding checks for passengers who have already checked in and recording the latest data of the boarding checks in a client database, so that the passengers can still inquire and use the boarding checks in a network-free environment. According to the invention, a large amount of paper resources can be saved, the check-in efficiency of passengers can be effectively improved, the working pressure of on-site workers is relieved, and the riding experience of the passengers is optimized.

The utility model discloses a novel simulation flight rocker, which belongs to the technical field of flight rockers and comprises a horizontal supporting rod, a first vertical supporting rod is fixedly connected to one end of the top of the horizontal supporting rod in the Y-axis direction, and an operating rod body is movably connected to the top of an operating rod base support. Two damping assemblies are installed on the top of the operating rod base support, a plurality of damping assemblies are installed on the top of the horizontal supporting rod, a foot rudder assembly is installed at the other end of the top of the horizontal supporting rod in the Y-axis direction, and a throttle lever assembly is installed on one side of one screen plate in the X-axis direction. According to the utility model, by designing the damping assembly and the throttle lever assembly, when a user uses the flight rocker, hydraulic damping rods can be added among rotating joints by using the flight rocker, so that torque feedback felt by the user in simulated flight control is increased, the operation hand feeling is more real, and the simulated flight experience feeling is greatly improved.

The utility model relates to an SEB-eFX / eX2 testboard for an airplane passenger cabin seat, and belongs to the technical field of airplane SEB-eFX / eX2 system testing. Comprising a test panel, a test host, a touch screen, a plurality of IO board cards, RS-232 terminals and a power supply, and the plurality of IO board cards connect the test host with a test part through a connector and a connecting line; the test parts are connected with the test board, so that the test parts can be detected, various function tests and troubleshooting can be carried out, convenience is provided for testing, normal use of the SEB-eFX / eX2 system of the passenger cabin seat of the airplane is ensured, and the service quality and the flight experience of passengers are improved.

The embodiment of the invention provides an intelligent flight plan making system and method, and belongs to the technical field of data processing. The intelligent flight plan making system comprises a flight training outline module, a pilot management module, a maintenance management module, a meteorological monitoring module, an airspace management module and a route management module. The flight training outline module is used for storing basic flight information and subject content of flight skill training; the pilot management module is used for managing pilot information and recording flight experience; the maintenance management module is used for managing aircraft information, recording aircraft maintenance states and analyzing aircraft fault frequency data; the meteorological monitoring module is used for collecting meteorological data and storing historical weather information; the airspace management module is used for providing airspace dynamic information; the route management module is used for providing path information. According to the invention, the data of each module can be automatically summarized, manual data entry and summarization are not needed, the data processing efficiency and accuracy are improved, and the overall efficiency of flight plan management is improved.

The utility model relates to the technical field of unmanned aerial vehicle experience cabins, and particularly discloses an unmanned aerial vehicle flight experience cabin which comprises a cabin body, a cabin top is arranged at the upper end of the cabin body, a parking apron is installed on the cabin top, a control seat is arranged in the cabin body, and at least one side face of the cabin body is provided with an opening. A folding door assembly is installed in the opening so that the opening can be opened or closed. According to the unmanned aerial vehicle flight experience cabin, the folding door assembly is arranged at the opening of the cabin body, and when the folding door assembly is opened, the opening area of the opening is maximized, so that the unmanned aerial vehicle flight experience cabin is more suitable for being used in a multi-person scene, the phenomenon that people are squeezed due to the fact that multiple people enter and exit is avoided, and the fun of the unmanned aerial vehicle flight experience cabin is greatly improved.

The application discloses a kind of based on skin electric signal's flight student psychological stress data acquisition method, it is related to machine learning technical field.The technical points of the present application include: collecting the skin electric signal of multiple flight students when flight simulation training, as physiological signal data set;The motion artifact removal is carried out to the skin electric signal collected;The skin electric signal after removing artifact is carried out frequency domain, time domain and nonlinear feature extraction, forms skin electric signal feature set;According to skin electric signal feature set, train psychological stress data acquisition model based on parallel neural network;The skin electric signal of new flight student is input in the psychological stress data acquisition model trained when flight simulation training, and the psychological stress data of new flight student is acquired.The present application can accurately express the fluctuation of psychological state of flight student when carrying out simulation flight training, help flight student summarizes flight experience, and provides help for subsequent flight training of flight student.

The invention discloses a system integrating various devices to guarantee low-altitude flight safety and improve flight experience, the system comprises a CPU control processing system and a battery electrically connected with the CPU control processing system and used for supplying power to the CPU control processing system, the CPU control processing system comprises a subsystem and a high-performance multi-core CPU, the subsystem comprises a microwave annunciator, a flash device, a parachute triggering device, a gyroscope balancing device, an automatic alarm device, a satellite positioning device, an optical radar and a health monitoring device; according to the invention, various devices with different functions, such as the high-performance multi-core CPU, the microwave annunciator, the flash device, the parachute triggering device, the gyroscope balancing device, the automatic alarm device, the satellite positioning device, the optical radar and the health monitoring device, are integrated together, so that the complexity of the system is reduced, and the cooperative work efficiency among the devices is improved; and seamless joint among the functions is realized.

This utility model relates to the field of tabletop technology and discloses a multifunctional aviation seat dining table, including a tabletop, a screw adjustment mechanism, a hinge assembly, and a rotatable panel. The screw adjustment mechanism is installed inside the tabletop, and the rotatable panel is hinged to the screw adjustment mechanism. Turning a handwheel drives the screw adjustment mechanism to move, causing the rotatable panel to rotate around the seat body, thereby adjusting the angle of the rotatable panel. The multifunctional aviation seat dining table provided by this utility model, through innovative design and reasonable structural layout, achieves both multifunctionality and high adjustability, providing passengers with a more convenient and comfortable flight experience.

1. Name of the product in this design: Flight Simulator (Two-person Frame Type). 2. Purpose of this design: for flight training and flight experience. 3. The key design feature of this product is its shape. 4. The image or photograph that best illustrates the design's key points: 3D view 1.

The utility model relates to an airplane PSU testboard, and belongs to the technical field of PSU testing. Comprising a test panel, a connector, a switch, an indicating lamp, a test hole, a signal generator and a power supply, a PCB is installed on the test panel, the connector, the switch, the indicating lamp and the test hole are all installed on the test panel, the connector, the switch, the indicating lamp and the test hole are all connected with the PCB, and the signal generator is connected with the PCB. The test hole is also connected with a signal generator, and the power supply supplies power to the test after voltage reduction of the transformer; the test board is convenient for testing, checking or troubleshooting the passenger service unit (PSU), ensures the normal use of the passenger service unit (PSU), ensures the flight service quality, and improves the flight experience of passengers.

The embodiment of the invention discloses a flight control method and device of an unmanned aerial vehicle, the unmanned aerial vehicle and a storage medium, and relates to the technical field of unmanned aerial vehicles. The method comprises the following steps: integrating the flight speed of the unmanned aerial vehicle to obtain an integral distance; when the integral distance exceeds a preset period distance, determining a distance variation between the unmanned aerial vehicle and the obstacle detected by the radar in an integral time period corresponding to the integral distance; determining an obstacle type according to the distance variation, and determining a flight strategy according to the obstacle type; and controlling the UAV to fly according to the flight strategy. According to the technical scheme provided by the embodiment of the invention, false signals can be effectively filtered, the obstacle type can be determined more accurately, the flight strategy can be determined in a targeted manner according to the obstacle type, unnecessary obstacle avoidance flight actions are reduced, energy consumption and flight efficiency loss caused by false alarms are reduced, and the flight experience is improved. And the flight efficiency of the unmanned aerial vehicle is improved.

1. The name of the design product: aircraft (parrot shuttle AeroPilotX). 2. The use of the design product: This product is designed for sports racing and low-altitude flight experience, suitable for flight performance, flight competition and individual flight entertainment activities in specific venues or open airspace. 3. The design points of the design product: the combination of shape and pattern. 4. The picture or photo that best shows the design points: perspective view 1.

1. Name of the product in this design: Powered Suspension Glider. 2. Intended use of this design: for aviation sports, recreational flying, and flight experiences. 3. The key design feature of this product is its shape. 4. The image or photograph that best illustrates the design's key points: a 3D model. 5. The bottom surface of this product is a part that is not easily seen or cannot be seen during use, so the bottom view is omitted.