CN110930812A - Control system for airplane simulation cockpit - Google Patents
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- G09B9/00—Simulators for teaching or training purposes
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Abstract
The embodiment of the invention discloses an airplane simulation cockpit control system, which comprises a computer auxiliary system, an interaction module, a physiological state detection module, an emergency shutdown module and an auxiliary display module, wherein the computer auxiliary system is connected with the interaction module; the computer-aided system comprises a server and a client, wherein the client presents a corresponding virtual flight scene according to training parameters set on the server by a user and presents the virtual flight scene to a current trainer through VR glasses; the interaction module is used for receiving an operation instruction input by a current trainer, and the client simulates the flight simulator to fly in a virtual flight scene according to the operation instruction; the physiological state detection module can be worn and used for monitoring the physiological parameters of the current trainer; the emergency shutdown module is used for resetting the flight simulator and locking the flight simulator when the flight simulator is in a fault state and/or the physiological parameter exceeds a preset parameter threshold value or a user trigger instruction is received.
Description
Technical Field
The invention relates to a flight simulator, in particular to an aircraft simulation cockpit control system.
Background
Simulation training, also called simulation, is an important subject in military and aerospace, and is a method for modeling in military and then simulating a tactical office, a strategy and a tactical plan by using a simulation technology. This method applies the view of the system theory and utilizes various modeling methods such as mathematical modeling. In practice, the simulation training has a great guiding function for the command of military operation. Particularly, the cultivation cost of a pilot is extremely expensive, the cultivation cost of the pilot of a modern fighter aircraft reaches at least 2000 cases, the light aviation oil consumes 2000 tons, the oil cost occupies 1400 tens of thousands, the qualified pilot trains at least 1000 hours of flight records every year, and the loss of exercise ammunition and the abrasion and part replacement of a flight simulator in a cabin are also realized. Each training is of money, the price of the pilot exceeds the weight gold, and a pilot who can fight a stick spends at least 2 times his weight gold. Besides the cost, there is a problem in safety.
A flight simulator, in a broad sense, is a machine used to simulate the flight of an aircraft. The simulator can reproduce an aircraft and an air environment and can operate, and energy consumption is much lower than that of real flight. If the flight simulator can be used for completing part of training, the safety factor in real flight can be improved, and the training cost of a pilot can be reduced. There are many flight simulators in the existing market, but mostly just provide one before the seat and control the platform and let the people experience the operation, and is few with user's interaction, lacks feedback data, and training effect can not obtain too big promotion.
Disclosure of Invention
In view of the above technical problems, an embodiment of the present invention provides an aircraft simulated cockpit control system.
The embodiment of the invention provides an airplane simulation cockpit control system, which comprises a computer auxiliary system, an interaction module, a physiological state detection module, an emergency shutdown module and an auxiliary display module, wherein the computer auxiliary system is respectively communicated with the interaction module, the physiological state detection module, the emergency shutdown module and the auxiliary display module;
the computer-aided system comprises a server and a client, wherein the client comprises VR glasses, and the client presents a corresponding virtual flight scene according to training parameters set on the server by a user and presents the virtual flight scene to a current trainer through the VR glasses;
the interactive module is used for receiving an operation instruction input by a current trainer, the client simulates a flight simulator to fly in the virtual flight scene according to the operation instruction, and the interactive module is provided with a seat;
the physiological state detection module can be worn, and is used for monitoring the physiological parameters of the current trainer;
the emergency shutdown module is used for recovering the flight simulator to a preset initial position of the flight simulator in the virtual flight scene or a horizontal position which is closest to the current position of the flight simulator in the virtual flight scene when the flight simulator is in a fault state and/or the physiological parameter exceeds a preset parameter threshold value or a user trigger instruction is received, and locking the flight simulator;
the auxiliary display module is used for displaying the flight parameters of the flight simulator and/or the state information of the flight simulator and presenting the flight parameters and/or the state information to the current trainer through the VR glasses.
Optionally, the training parameters include one or more of model information, environmental parameters, wind parameters, characteristic parameters, special case training patterns, hardware detection, grouping information, data storage information, and weapons ammunition information;
wherein the environmental parameters are used to indicate terrain information and weather information of the virtual flying scene;
the wind parameters are used for indicating wind directions and/or wind speeds of different height positions in the virtual flight scene;
the characteristic parameter is used for indicating whether a virtual airplane is set in the virtual flight scene;
the special situation training mode comprises the following steps: the training mode comprises a training mode in which no fault occurs in the flight process of the flight simulator, a training mode in which a random fault occurs in the flight process of the flight simulator, and a training mode in which a preset fault occurs in the flight process of the flight simulator;
the grouping information includes: identity information of the current trainer and/or class information of the current trainer;
the data storage information includes: current training parameters, performance data and physiological parameters of the current trainer;
the weapon ammunition information comprises at least one of mounted missile training, air launching target hitting training, air combat training and tactical drilling.
Optionally, the interactive module includes a main body, a steering wheel, a throttle, a control lever and a foot pedal, and the seat, the steering wheel, the throttle, the control lever and the foot pedal are disposed on the main body;
the steering wheel is used for controlling an aileron of the flight simulator;
the throttle is used for controlling the speed of the flight simulator;
the control rod is used for controlling an elevator of the flight simulator;
the foot peg is used to control a rudder of the flight simulator.
Optionally, the physiological state detecting module includes a heart rate monitoring module and a blood pressure monitoring module.
Optionally, the aircraft simulated cockpit control system further includes a wireless data receiving terminal, the wireless data receiving terminal communicates with the computer-assisted system, and the computer-assisted system sends the physiological parameter monitored by the physiological status detecting module to the wireless data receiving terminal.
Optionally, the physiological state detection module is a smart band.
Optionally, the computer-assisted system outputs alarm information and starts the emergency shutdown module when the heart rate monitored by the heart rate monitoring module exceeds a preset heart rate threshold, or the blood pressure monitored by the blood pressure monitoring module exceeds a first preset blood pressure threshold, or a low pressure value monitored by the blood pressure monitoring module is lower than a second preset blood pressure threshold.
Optionally, the aircraft simulated cockpit control system includes a voice dialog module and an operation signal lamp, and the computer-assisted system outputs the alarm information in a voice manner through the voice dialog module and controls the operation signal lamp to display a preset color when the heart rate monitored by the heart rate monitoring module exceeds a preset heart rate threshold value or the blood pressure monitored by the blood pressure monitoring module exceeds a first preset blood pressure threshold value or the low pressure value monitored by the blood pressure monitoring module is lower than a second preset blood pressure threshold value, where the preset color is used for prompting that the heart rate monitored by the heart rate monitoring module exceeds the preset heart rate threshold value or the blood pressure monitored by the blood pressure monitoring module exceeds the first preset blood pressure threshold value or the low pressure value monitored by the blood pressure monitoring module is lower than the second preset blood pressure threshold value.
Optionally, the auxiliary display system includes an instrument panel of the flight simulator disposed on the interaction module and an aircraft state display module, where the instrument panel is used to display flight parameters of the flight simulator;
the display module is used for displaying the state information of the flight simulator.
Optionally, the flight parameter package: altitude, speed, and geographic location.
In the technical scheme provided by the embodiment of the invention, a vivid cockpit system is constructed by combining a virtual reality technology with software and hardware equipment; meanwhile, the physiological parameters of the trainee are monitored in real time through the physiological state detection module and transmitted to the server, so that compared with the prior art of liquid crystal display, immersive experience, contextual experience and participatory experience, the simulation training effect of the trainee can be intuitively and comprehensively known in the embodiment of the invention, and the simulation training effect is improved.
Drawings
FIG. 1 is a schematic diagram of an embodiment of an aircraft simulated cockpit control system according to an embodiment of the present invention;
FIG. 2 is a schematic diagram of an embodiment of a computer-aided system according to an embodiment of the present invention;
FIG. 3 is a schematic diagram of another embodiment of a computer-assisted system according to an embodiment of the present invention;
FIG. 4 is a diagram of an interaction module according to an embodiment of the present invention;
FIG. 5 is a schematic view of another embodiment of a simulated cockpit control system of an aircraft according to an embodiment of the present invention;
FIG. 6 is a schematic view of another embodiment of a simulated cockpit control system of an aircraft according to an embodiment of the present invention;
FIG. 7 is a schematic diagram of an exemplary embodiment of an aircraft simulation cockpit control system operating process;
fig. 8 is a schematic diagram of another embodiment of the aircraft simulated cockpit control system according to the embodiment of the invention.
Reference numerals:
1: a computer-assisted system; 11: a server; 12: a client; 121: VR glasses; 2: an interaction module; 3: a physiological state detection module; 4: an emergency shutdown module; 5: an auxiliary display module; 51: an instrument panel; 52: an aircraft state display module; 6: an in-cabin video monitoring module; 7: a voice dialog module; 8: operating a signal lamp; 9: and a wireless data receiving end.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
It should be noted that the following embodiments may be combined without conflict.
Referring to fig. 1 and fig. 2, the aircraft cabin simulation control system according to the embodiment of the present invention may include a computer-aided system 1, an interaction module 2, a physiological status detection module 3, an emergency shutdown module 4, and an auxiliary display module 5, wherein the computer-aided system 1 is in communication with the interaction module 2, the physiological status detection module 3, the emergency shutdown module 4, and the auxiliary display module 5, respectively.
The computer-assisted system 1 includes a server 11 and a client 12, the client 12 includes VR glasses 121, and the client 12 presents a corresponding virtual flight scene according to training parameters set on the server 11 by a user, and presents the virtual flight scene to a current trainer through the VR glasses 121. The interactive module 2 is used for receiving an operation instruction input by a current trainer, the client 12 simulates a flight simulator to fly in a virtual flight scene according to the operation instruction, and the interactive module 2 is provided with a seat for the current trainer to use. The physiological state detection module 3 can be worn, and the physiological state detection module 3 is used for monitoring the physiological parameters of the current trainer. The emergency shutdown module 4 is configured to, when the flight simulator is in a fault state and/or the physiological parameter exceeds a preset parameter threshold value, or when a user trigger instruction is received, restore the flight simulator to an initial position of the preset flight simulator in a virtual flight scene or a horizontal position closest to a current position of the flight simulator in the virtual flight scene, and lock the flight simulator. The auxiliary display module 5 is used for displaying the flight parameters of the flight simulator and/or the state information of the flight simulator, and presenting the flight parameters and/or the state information to the current trainer through the VR glasses 121. In the embodiment of the present invention, the initial position is a preset position.
The aircraft simulation cockpit control system of the embodiment of the invention adopts the virtual reality technology to be combined with software and hardware equipment to construct a vivid cockpit system; meanwhile, the physiological parameters of the trainee are monitored in real time through the physiological state detection module 3 and transmitted to the server 11, so that the effect of the simulation training on the trainee can be intuitively and comprehensively known, and the simulation training effect is improved.
Optionally, the computer-aided system 1 includes a plurality of hosts, one of the hosts is used as the server 11, the other hosts are used as the clients 12, the plurality of clients 12 are controlled by the server 11, and accordingly, the number of the interaction module 2, the physiological status detection module 3, the emergency shutdown module 4 and the auxiliary display module 5 is matched with the number of the clients 12, so that a plurality of trainers can perform simulated training at the same time.
A user (e.g., an operator) may set a training parameter corresponding to each client 12 on the server 11, so that each client 12 presents a corresponding virtual flight scenario according to the respective training parameter. Optionally, the training parameters may include one or more of model information, environmental parameters, wind parameters, characteristic parameters, idiosyncratic training patterns, hardware detection, grouping information, data storage information, and weapons ammunition information. After the model information is set, the client 12 presents the flight simulator corresponding to the currently set model information. The environmental parameters are used to indicate terrain information and weather information for the virtual flight scenario. The wind power parameters are used for indicating wind directions and/or wind speeds of different height positions in the virtual flight scene, so that the resistance or thrust of the flight simulator at different heights is influenced, and the flight simulator is more appropriate to the real flight environment. The characteristic parameters are used for indicating whether to set up a virtual airplane or an in-cabin flight simulator formation in a virtual flight scene so as to increase the difficulty of simulation training. The special situation training mode comprises the following steps: the training mode is that the flight simulator flies normally in the flight process, the hardware structure and software of the flight simulator run normally, the training mode is that the flight simulator flies randomly in the flight process, the flight simulator flies randomly and randomly generates special conditions, the flight simulator has random faults in the flight process, the training mode is that the flight simulator has preset faults in the flight process, the training mode is that the flight simulator has specific conditions, and the flight simulator has specific faults in the flight process, so that the special condition training is very important, how to deal with various situations encountered by the pilot in flight, and the special condition training also provides main data for the physiological state detection module 3. The hardware detection mainly comprises the steps of firstly detecting whether each hardware device is normally connected and returned when the system is operated, and resetting the state of the hardware device. The grouping information may include: optionally, the setting of the grouping information may set the shift entry and the equipment arrangement, and record the feedback and the record of the relevant data such as the corresponding machine number, the name, the convenience score and the like to the trainers participating in the training. The data storage information includes: the current training parameters, the performance data and the physiological parameters of the current trainer, the data access information, namely all parameters set by the server and the performance after training, are accessed through the database, the defects of the trainer are favorably analyzed, the data can be used for training, and the qualified pilot who can win the battle can be achieved. The weapon ammunition information comprises at least one of mounted missile training, air launching target hitting training, air combat training and tactical drilling, wherein the mounted missile training, the air launching target hitting training, the air combat training and the tactical drilling are all existing tactical training modes; of course, the weapon ammunition information can also be set into other tactical training modes.
It will be appreciated that when not set, the training parameters select default parameters.
Referring to fig. 4, the interactive module 2 may include a main body, a steering wheel, a throttle, a lever, and a pedal, and the seat, the steering wheel, the throttle, the lever, and the pedal are disposed on the main body. The steering wheel, the accelerator, the control rod and the pedals are arranged in front of the seat, and a trainer can operate the steering wheel, the accelerator, the control rod and the pedals by sitting on the seat so as to simulate the control of the flight simulator. Specifically, the steering wheel is used to control the ailerons of the flight simulator, the throttle is used to control the speed of the flight simulator, the joystick is used to control the elevator of the flight simulator, and the pedals are used to control the rudder of the flight simulator. It should be noted that the steering wheel, the throttle, the control lever and the foot pedal are 1: 1, physical simulation.
Optionally, the physiological state detecting module 3 includes a heart rate monitoring module and a blood pressure monitoring module, wherein the heart rate monitoring module is configured to monitor the heart rate of the current trainer, and the blood pressure monitoring module is configured to monitor the blood pressure of the current trainer; of course, the physiological status detection module 3 may also include other structures for monitoring the physiological parameters of the trainer.
Referring to fig. 5, in some embodiments, the physiological status detecting module 3 is a smart band; of course, in other embodiments, the physiological status detection module 3 may be other types of wearable devices.
Further, please refer to fig. 5 again, the aircraft cabin simulation control system may further include a wireless data receiving terminal 9, the wireless data receiving terminal 9 is in communication with the computer-aided system 1, and the computer-aided system 1 sends the physiological parameters monitored by the physiological status detecting module 3 to the wireless data receiving terminal 9, so that other devices can obtain the physiological parameters of the current trainer.
The computer-aided system 1 of this embodiment outputs alarm information when the heart rate monitored by the heart rate monitoring module exceeds a preset heart rate threshold or the high pressure value monitored by the blood pressure monitoring module exceeds a first preset blood pressure threshold or the low pressure value monitored by the blood pressure monitoring module is lower than a second preset blood pressure threshold, and starts the emergency shutdown module 4. The preset heart rate threshold value is a limit value of a normal heart rate of a human body, the first preset blood pressure threshold value is a limit value of a normal high pressure of the human body, and the second preset blood pressure threshold value is a limit value of a normal low pressure of the human body.
Optionally, referring to fig. 6, the aircraft simulated cockpit control system may further include a voice dialog module 7 and an operation signal lamp 8, when the heart rate monitored by the heart rate monitoring module exceeds a preset heart rate threshold or the blood pressure monitored by the blood pressure monitoring module exceeds a first preset blood pressure threshold or the low pressure value monitored by the blood pressure monitoring module is lower than a second preset blood pressure threshold, the computer-assisted system 1 outputs alarm information in a voice manner through the voice dialog module 7, and controls the operation signal lamp 8 to display a preset color, where the preset color is used to prompt that the heart rate monitored by the heart rate monitoring module exceeds the preset heart rate threshold or the low pressure value monitored by the blood pressure monitoring module exceeds the first preset blood pressure threshold or the low pressure value monitored by the blood pressure monitoring module is lower than the second preset blood pressure. Furthermore, the voice dialogue module 7 enables voice dialogue for the current trainer and operator.
Referring to fig. 7, when the aircraft simulated cockpit control system is operating normally (i.e. there is no software and hardware fault in the aircraft simulated cockpit control system), the operation signal lamp 8 flashes a green lamp; when a first type of software and hardware faults occur in the aircraft simulated cabin control system, the operation signal lamp 8 displays a yellow lamp; when a trainer has physical abnormality (the heart rate exceeds a preset heart rate threshold value, the blood pressure exceeds a first preset blood pressure threshold value or a low pressure value monitored by the blood pressure monitoring module is lower than a second preset blood pressure threshold value), or a second type of software and hardware faults occur in an airplane simulation cockpit control system, the signal lamp 8 is operated to display a red light, an alarm is given, and the emergency shutdown module 4 is started to execute an emergency shutdown program. Referring to fig. 6 again, the aircraft simulated cockpit control system may further include an in-cabin video monitoring module 6, and an operator may observe the state of the trainer in real time through the in-cabin video monitoring module 6; when the aircraft simulated cockpit control system is in an emergency, the aircraft simulated cockpit control system can automatically trigger the emergency shutdown module 4, recover the flight of the flight simulator to the initial position of the preset flight simulator in the virtual flight scene or the horizontal position which is closest to the current position of the flight simulator in the virtual flight scene as far as possible, and keep the flight simulator in a locked state; when the trainer finds the body state is bad, the emergency shutdown module 4 can be manually started (at this time, the emergency shutdown module 4 receives a user trigger instruction) to control the system to return to the initial state. Optionally, the repair time for the first type of hardware and software failure is less than the repair time for the second type of hardware and software failure. When the flight simulator remains in the locked state, the flight of the flight simulator cannot be simulated and controlled.
Referring to fig. 8, the auxiliary display system may include a dashboard 51 of the flight simulator disposed on the interactive module 2 and an aircraft status display module 52, where the dashboard 51 is used to display flight parameters of the flight simulator, and optionally, the flight parameter package: altitude, speed, and geographic location; the display module is used for displaying the state information of the flight simulator, such as a normal working state and a fault state (the fault type can be displayed). In the embodiment of the invention, 1: 1, simulating and restoring an instrument panel and an aircraft state display module of a flight simulator in a cabin, displaying information such as the flying height, speed and geographic position of the flight simulator, and visually checking real-time data of the instrument panel 51 in the cabin by a trainer in VR virtual glasses through a camera of the VR virtual glasses; in the training process of a trainer, the trainer can visually know the mechanical and software running states of the flight simulator through the flight simulator state display module, and can ask an operator for help at any time when an abnormal problem occurs.
The above examples are only intended to illustrate the technical solution of the present invention, but not to limit it; although the present invention has been described in detail with reference to the foregoing embodiments, it will be understood by those of ordinary skill in the art that: the technical solutions described in the foregoing embodiments may still be modified, or some technical features may be equivalently replaced; and such modifications or substitutions do not depart from the spirit and scope of the corresponding technical solutions of the embodiments of the present invention.
Claims (10)
1. An aircraft simulated cockpit control system is characterized in that the aircraft simulated cockpit computer-aided system (1) comprises a computer-aided system (1), an interaction module (2), a physiological state detection module (3), an emergency shutdown module (4) and an auxiliary display module (5), wherein the computer-aided system (1) is respectively communicated with the interaction module (2), the physiological state detection module (3), the emergency shutdown module (4) and the auxiliary display module (5);
the computer-aided system (1) comprises a server (11) and a client (12), wherein the client (12) comprises VR glasses (121), the client (12) presents a corresponding virtual flight scene according to training parameters set on the server (11) by a user, and presents the virtual flight scene to a current trainer through the VR glasses (121);
the interaction module (2) is used for receiving an operation instruction input by a current trainer, the client (12) simulates a flight simulator to fly in the virtual flight scene according to the operation instruction, and the interaction module (2) is provided with a seat;
the physiological state detection module (3) is wearable, and the physiological state detection module (3) is used for monitoring physiological parameters of a current trainer;
the emergency shutdown module (4) is configured to, when the flight simulator is in a fault state and/or the physiological parameter exceeds a preset parameter threshold value, or a user trigger instruction is received, restore the flight simulator to a preset initial position of the flight simulator in the virtual flight scene or a horizontal position closest to the current position of the flight simulator in the virtual flight scene, and lock the flight simulator;
the auxiliary display module (5) is used for displaying flight parameters of the flight simulator and/or state information of the flight simulator and presenting the flight parameters and/or the state information to a current trainer through the VR glasses (121).
2. The aircraft simulated cockpit control system of claim 1 where said training parameters include one or more of model information, environmental parameters, wind parameters, performance parameters, idiosyncratic training patterns, hardware detection, grouping information, data storage information, and weapons ammunition information;
wherein the environmental parameters are used to indicate terrain information and weather information of the virtual flying scene;
the wind parameters are used for indicating wind directions and/or wind speeds of different height positions in the virtual flight scene;
the characteristic parameter is used for indicating whether a virtual airplane is set in the virtual flight scene;
the special situation training mode comprises the following steps: the training mode comprises a training mode in which no fault occurs in the flight process of the flight simulator, a training mode in which a random fault occurs in the flight process of the flight simulator, and a training mode in which a preset fault occurs in the flight process of the flight simulator;
the grouping information includes: identity information of the current trainer and/or class information of the current trainer;
the data storage information includes: current training parameters, performance data and physiological parameters of the current trainer;
the weapon ammunition information comprises at least one of mounted missile training, air launching target hitting training, air combat training and tactical drilling.
3. An aircraft simulated cockpit control system according to claim 1 where said interaction module (2) comprises a main body, a steering wheel, a throttle, a joystick and a foot pedal, said seat, said steering wheel, said throttle, said joystick and said foot pedal being provided on said main body;
the steering wheel is used for controlling an aileron of the flight simulator;
the throttle is used for controlling the speed of the flight simulator;
the control rod is used for controlling an elevator of the flight simulator;
the foot peg is used to control a rudder of the flight simulator.
4. The aircraft cabin control simulation system according to claim 1, wherein the physiological state detection module (3) comprises a heart rate monitoring module and a blood pressure monitoring module.
5. The aircraft cabin control system according to claim 4, further comprising a wireless data receiving terminal (9), wherein the wireless data receiving terminal (9) is in communication with the computer-assisted system (1), and the computer-assisted system (1) transmits the physiological parameters monitored by the physiological status detection module (3) to the wireless data receiving terminal (9).
6. The control system of an aircraft simulated cockpit according to claim 1 or 4 or 5 where the physiological state detection module (3) is a smart bracelet.
7. The aircraft cabin control simulation system according to claim 4, wherein the computer-assisted system (1) outputs an alarm message and activates the emergency shutdown module (4) when the heart rate monitored by the heart rate monitoring module exceeds a preset heart rate threshold value or the blood pressure monitored by the blood pressure monitoring module exceeds a first preset blood pressure threshold value or the low pressure value monitored by the blood pressure monitoring module is lower than a second preset blood pressure threshold value.
8. The aircraft simulated cockpit control system of claim 7 comprising a voice dialog module (7) and a running light (8), when the heart rate monitored by the heart rate monitoring module exceeds a preset heart rate threshold value or the blood pressure monitored by the blood pressure monitoring module exceeds a first preset blood pressure threshold value or the low pressure value monitored by the blood pressure monitoring module is lower than a second preset blood pressure threshold value, the alarm information is output in a voice mode through the voice dialogue module (7), and the operation signal lamp (8) is controlled to display a preset color, the preset color is used for prompting that the heart rate monitored by the heart rate monitoring module exceeds a preset heart rate threshold value or the blood pressure monitored by the blood pressure monitoring module exceeds a first preset blood pressure threshold value or a low pressure value monitored by the blood pressure monitoring module is lower than a second preset blood pressure threshold value.
9. An aircraft cabin simulation control system according to claim 1, characterized in that the auxiliary display system comprises an instrument panel (51) of the flight simulator provided on the interaction module (2) and an aircraft status display module (52), the instrument panel (51) being adapted to display flight parameters of the flight simulator;
the display module is used for displaying the state information of the flight simulator.
10. The aircraft simulated cockpit control system of claim 9 where said flight parameter package is: altitude, speed, and geographic location.
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| CN113409649A (en) * | 2021-06-17 | 2021-09-17 | 中国人民解放军空军特色医学中心 | Vestibular inclination illusion simulation method and device and flight illusion simulator |
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