CN113721479A - Unmanned aerial vehicle simulation training system - Google Patents
Unmanned aerial vehicle simulation training system Download PDFInfo
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Abstract
The invention provides an unmanned aerial vehicle simulation training system, which comprises: the system comprises a three-dimensional simulation unit, a ground station unit and a training evaluation unit; the three-dimensional simulation unit is used for carrying out flight simulation according to the unmanned aerial vehicle flight control data input by the ground station unit and displaying a route, a first visual angle, a third visual angle and a three-dimensional simulation environment on the intelligent display module; the ground station unit is used for controlling training personnel to input flight control instructions and flight parameters and managing the sending states of the telemetering data, flight tracks and control instruction instructions; the training evaluation unit is used for receiving flight parameters of the virtual unmanned aerial vehicle of the three-dimensional simulation unit, realizing flight training in different simulation environments according to set subjects and scene parameters, recording and replaying data of the flight training, and reading training operation data to evaluate training operation scores.
Description
Technical Field
The invention relates to the technical field of unmanned aerial vehicle training, in particular to an unmanned aerial vehicle simulation training system.
Background
The control of the pilotless aircraft is a relatively complex process, and has relatively high requirements on control personnel, so the control personnel can carry out simulation training through the training simulation system, the cost can be saved, and unnecessary loss of the pilotless aircraft caused by unskilled control can be avoided. The existing unmanned aerial vehicle training system has single training mode, lower efficiency and high cost, is difficult to better meet the training requirement,
in conclusion, the unmanned aerial vehicle simulation training system which can effectively assist an unmanned aerial vehicle operator to perform multi-mode and multi-scene training and has good expansibility is provided, and is a problem which needs to be solved urgently by technical personnel in the field.
Disclosure of Invention
In order to solve the problems and requirements mentioned above, the present solution provides an unmanned aerial vehicle simulation training system, which can solve the above technical problems by adopting the following technical solutions.
In order to achieve the purpose, the invention provides the following technical scheme: an unmanned aerial vehicle simulated training system comprising: the system comprises a three-dimensional simulation unit, a ground station unit and a training evaluation unit;
the three-dimensional simulation unit is used for carrying out flight simulation according to the unmanned aerial vehicle flight control data input by the ground station unit and displaying a route, a first visual angle, a third visual angle and a three-dimensional simulation environment on the intelligent display module;
the ground station unit is used for controlling training personnel to input flight control instructions and flight parameters and managing the sending states of the telemetering data, flight tracks and control instruction instructions;
the training evaluation unit is used for receiving flight parameters of the virtual unmanned aerial vehicle of the three-dimensional simulation unit, realizing flight training in different simulation environments according to set subjects and scene parameters, recording and playing back data of the flight training in different simulation environments, and reading training operation data to evaluate training operation scores.
Further, the three-dimensional simulation unit comprises a simulation module, the simulation module receives a remote control instruction to change the flight attitude of the unmanned aerial vehicle, an equation and a control law of the aircraft are established by utilizing the pneumatic parameters, the wing section parameters and the power parameters of the aircraft according to a FlightGear2018 platform, a mathematical model is established, the flight attitude and the flight distance parameters of the aircraft are generated by taking time as a coordinate simulation, and then a flight control computer, a navigation computer, an aircraft power and pneumatic system and a steering engine equipment system are simulated by adopting a mathematical simulation method.
Furthermore, the three-dimensional simulation unit further comprises a data receiving module, wherein the data receiving module is used for receiving an input flight interaction instruction and set parameters, the flight interaction instruction comprises flight speed, attitude and height, and the set parameters comprise waypoint information and simulated environment parameter information.
Furthermore, the ground station unit comprises a controller, an interface module, a control panel, a data transmission antenna, a host and a charging module;
the control panel comprises a rocker module, a first intelligent interaction module and a plurality of groups of control buttons, the rocker module comprises a speed and direction control rocker and a flight attitude control rocker, the speed and direction control rocker is shifted up and down to control an accelerator, namely to control the speed, the left and right are shifted to control the direction, the flight attitude control rocker is shifted up and down to control the pitching of the airframe, the left and right are used for controlling the rolling of the airframe, the first intelligent interaction module is used for inputting flight control instructions, flight route planning instructions and displaying telemetering data, flight tracks and control instruction sending states, the first intelligent interaction module inputs the flight route planning instructions and comprises simple flight route planning and automatic flight route planning, the plurality of groups of control buttons comprise a power supply button, a starting button, a locking/unlocking button, a manual button, an automatic button, a self-defining button and a return flight button, the rocker module, the first intelligent interaction module and the plurality of groups of control buttons are all connected with the controller;
the interface module comprises an HDMI high-definition interface, a USB3.0 interface and a network interface, the interface module and the controller are both connected with the host, and the host is connected with the three-dimensional simulation unit and used for combining flight control parameters with the virtual unmanned aerial vehicle of the simulation module through an interface protocol;
the charging module is used for charging the ground station unit.
Furthermore, the ground station unit further comprises an electric quantity display module and a heat dissipation module, the electric quantity display module is used for displaying the residual electric quantity of the ground command unit, the electric quantity display module comprises an electric quantity display, the heat dissipation module comprises a pair of heat dissipation fans, the pair of heat dissipation fans are electrically connected with the controller, and when the system temperature exceeds a set temperature threshold value, the controller controls the pair of heat dissipation fans to rotate for heat dissipation.
Furthermore, the training evaluation unit comprises a selection module, a switching module, a data management module and a parameter receiving module;
the selection module is used for selecting different types and training subjects of the virtual unmanned aerial vehicle and starting the view of the corresponding type;
the switching module is used for switching between an automatic mode and a manual mode according to a state switching signal sent by the flight control unit, displaying the mode of the current state on a second intelligent interaction module of the console, and when the mode is in the manual mode, the model is driven by remote sensing data; when the model is in the automatic mode state, the model receives data sent by the ground station to drive the flight;
the data management module is used for recording and updating flight data, playing back the data and monitoring the flight data, and comprises a storage database, a recording control module, a data supervision module and an initialization module, wherein the storage database is used for storing the data in the model flight according to a storage list, the recording control module comprises a recording data/finishing recording button and a storage selection module, the recording data/finishing recording button is controlled, the system starts to record the flight data, at the moment, the training personnel is controlled to start operating the airplane flight, the recording data is required to be finished, the recording data/finishing recording button is controlled again, when the data is required to be stored, the training personnel is controlled to input the name of the data through the storage selection module to store the name, if the name is not input, the data is stored as a default data name, when the data do not need to be stored, the training personnel is controlled to select to cancel the storage through the storage selection module, the data supervision module is used for carrying out data playback according to a data playback instruction, deleting the recorded data according to a data deletion instruction, monitoring the yaw angle, the roll angle, the course angle and the height of the virtual unmanned aerial vehicle and indicating a data curve of the airspeed through the second intelligent interaction module, and the initialization module is used for initializing the data and the view;
the parameter receiving module is used for receiving an initialization instruction, a data recording updating instruction, a data playback instruction and an instruction for simulating wind speed and wind direction input by a training person through the second intelligent interaction module.
Furthermore, the flight control unit comprises a vertical flight knob, a pause switch, a control rod and a plurality of groups of control switches, wherein the vertical flight knob and the pause switch are connected with the controller, after the visual scene is started and initialized, the pause switch is pushed to start the model clock, training personnel are controlled to rotate the vertical flight knob to enable the airplane to take off vertically, when the height meets the requirement, the vertical flight knob can be rotated to a zero position, and the plurality of groups of control switches comprise a model selection switch, a visual scene starting switch, an initialization switch, a subject selection switch, a data recording/end recording switch, a data playback/end playback switch and a manual/automatic switching switch.
Furthermore, the training evaluation unit further comprises a score evaluation module, and the flight operation data read by the score evaluation module is compared and judged according to a set scoring rule to obtain a training score.
According to the technical scheme, the invention has the beneficial effects that: the invention can effectively assist the unmanned aerial vehicle control personnel to carry out multi-mode and multi-scene training and has good expansibility.
In addition to the above objects, features and advantages, preferred embodiments of the present invention will be described in more detail below with reference to the accompanying drawings so that the features and advantages of the present invention can be easily understood.
Drawings
In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings used in the description of the embodiments of the present invention or the prior art will be briefly described, wherein the drawings are only used for illustrating some embodiments of the present invention and do not limit all embodiments of the present invention thereto.
Fig. 1 is a schematic diagram of a composition structure of an unmanned aerial vehicle simulation training system of the present invention.
Fig. 2 is a schematic view of the composition structure of the control panel according to the present invention.
Fig. 3 is a schematic structural diagram of the flight control unit according to the present invention.
FIG. 4 is a schematic diagram of a data management module according to the present invention.
Fig. 5 is a schematic diagram of a procedure for evaluating the performance of the unmanned aerial vehicle simulated training in this embodiment.
Fig. 6 is a schematic flow chart of a method for using the ground station unit in this embodiment.
Fig. 7 is a visual training interface under different simulation training scenarios in this embodiment.
FIG. 8 is a data administration interface for the training assessment process of the present invention.
FIG. 9 is a visual control interface of the ground station of the present invention.
Detailed Description
In order to make the objects, technical solutions and advantages of the embodiments of the present invention clearer, the technical solutions of the embodiments of the present invention will be clearly and completely described below with reference to the accompanying drawings of specific embodiments of the present invention. Like reference symbols in the various drawings indicate like elements. It should be noted that the described embodiments are only some embodiments of the invention, and not all embodiments. All other embodiments, which can be derived by a person skilled in the art from the described embodiments of the invention without any inventive step, are within the scope of protection of the invention.
The invention provides an unmanned aerial vehicle control simulation training equipment system, which can provide a dynamic simulation training means based on capacity and supporting combined combat drilling for an unmanned aerial vehicle system, and can be used for on-duty training and daily training of unmanned aerial vehicle system control personnel. As shown in fig. 1 to 4, the system includes: the system comprises a three-dimensional simulation unit, a ground station unit and a training evaluation unit; the three-dimensional simulation unit is used for carrying out flight simulation according to the unmanned aerial vehicle flight control data input by the ground station unit, displaying a flight line, a first visual angle, a third visual angle and a three-dimensional simulation environment on the intelligent display module, and the three-dimensional simulation unit is communicated with the ground station unit through an interface communication protocol. The flight control data includes data such as the position, attitude, direction, mode switch, speed of the unmanned aerial vehicle system.
The three-dimensional simulation unit comprises a simulation module, the simulation module receives a remote control instruction to change the flight attitude of the unmanned aerial vehicle, an equation and a control law of the aircraft are established by utilizing the pneumatic parameters, the wing section parameters and the power parameters of the aircraft according to a flight gear2018 platform to establish a mathematical model, the flight attitude and the flight distance parameters of the aircraft are generated by taking time as a coordinate simulation, and then a flight control computer, a navigation computer, an aircraft power and pneumatic system and a steering engine equipment system are simulated by adopting a mathematical simulation method. The three-dimensional simulation unit further comprises a data receiving module, wherein the data receiving module is used for receiving an input flight interaction instruction and set parameters, the flight interaction instruction comprises flight speed, attitude and height, and the set parameters comprise waypoint information and simulated environment parameter information.
The ground station unit is used for controlling training personnel to input flight control instructions and flight parameters and managing the sending states of the telemetering data, flight tracks and control instruction instructions. In this embodiment, the ground station unit is towards unmanned aerial vehicle command control personnel and control personnel, through friendly human-computer interface, accomplishes information display such as telemetering measurement data, flight track and instruction sending state, and controls and be provided with various command button and control rod training aids on the panel. Specifically, the ground station unit comprises a controller, an interface module, a control panel, a data transmission antenna, a host and a charging module; the control panel comprises a rocker module, a first intelligent interaction module and a plurality of groups of control buttons, the rocker module comprises a speed and direction control rocker and a flight attitude control rocker, the speed and direction control rocker is shifted up and down to control an accelerator, namely to control the speed, the left and right are shifted to control the direction, the flight attitude control rocker is shifted up and down to control the pitching of the airframe, the left and right are used for controlling the rolling of the airframe, the first intelligent interaction module is used for inputting flight control instructions, flight route planning instructions and displaying telemetering data, flight tracks and control instruction sending states, the first intelligent interaction module inputs the flight route planning instructions and comprises simple flight route planning and automatic flight route planning, the plurality of groups of control buttons comprise a power supply button, a starting button, a locking/unlocking button, a manual button, an automatic button, a self-defining button and a return flight button, the rocker module, the first intelligent interaction module and the plurality of groups of control buttons are all connected with the controller; the interface module comprises an HDMI high-definition interface, a USB3.0 interface and a network interface, the interface module and the controller are both connected with the host, the host is connected with the three-dimensional simulation unit and is used for combining flight control parameters with the virtual unmanned aerial vehicle of the simulation module through an interface protocol, and the controller transmits control signals of the control panel to the virtual unmanned aerial vehicle of the simulation module through the host, so that the control of the virtual unmanned aerial vehicle is realized; the charging module is used for charging the ground station unit. When the power key is pressed, the ground station starts to supply power to start running. When the ground station is powered on, the built-in computer host starts to operate by pressing the power-on key. The locking/unlocking button is pressed to be in an unlocking state, and is pressed again to be in a locking state; manual control is switched by using a manual button, and a rocker can be used for controlling the manual control; the automatic button is used for switching to automatic control, and the control is carried out according to the preset control; the user can customize the related functions through the user-defined buttons. And when the return button is pressed, the training target returns to the task starting point.
The ground station unit further comprises an electric quantity display module and a heat dissipation module, the electric quantity display module is used for displaying the residual electric quantity of the ground command unit, the electric quantity display module comprises an electric quantity display, the heat dissipation module comprises a pair of heat dissipation fans, the pair of heat dissipation fans are electrically connected with the controller, and when the temperature of the system exceeds a set temperature threshold value, the controller controls the pair of heat dissipation fans to rotate for heat dissipation.
The training evaluation unit is used for receiving flight control instructions and virtual unmanned aerial vehicle flight parameters from the three-dimensional simulation subsystem and the ground station subsystem through a network protocol, realizing flight training in different simulation environments according to set subjects and scene parameters, recording and playing back data of the flight training in different simulation environments, and reading training operation data to evaluate training operation scores.
Specifically, the training evaluation unit comprises a selection module, a switching module, a data management module and a parameter receiving module; the selection module is used for selecting different types and training subjects of the virtual unmanned aerial vehicle and starting the view of the corresponding type; the switching module is used for switching between an automatic mode and a manual mode according to a state switching signal sent by the flight control unit, displaying the mode of the current state on a second intelligent interaction module of the console, and when the mode is in the manual mode, the model is driven by remote sensing data; when the model is in the automatic mode state, the model receives data sent by the ground station to drive the flight; the data management module is used for recording and updating flight data, playing back the data and monitoring the flight data, and comprises a storage database, a recording control module, a data supervision module and an initialization module, wherein the storage database is used for storing the data in the model flight according to a storage list, the recording control module comprises a recording data/finishing recording button and a storage selection module, the recording data/finishing recording button is controlled, the system starts to record the flight data, at the moment, the training personnel is controlled to start operating the airplane flight, the recording data is required to be finished, the recording data/finishing recording button is controlled again, when the data is required to be stored, the training personnel is controlled to input the name of the data through the storage selection module to store the name, if the name is not input, the data is stored as a default data name, when the data do not need to be stored, the training personnel is controlled to select to cancel the storage through the storage selection module, the data supervision module is used for carrying out data playback according to a data playback instruction, deleting recorded data according to a data deletion instruction, monitoring the yaw angle, the roll angle, the course angle and the height of the virtual unmanned aerial vehicle and indicating a data curve of the airspeed through the second intelligent interaction module, the second intelligent interaction module comprises an intelligent display screen, the initialization module is used for initializing data and a visual scene, a control system and a visual scene interface are initialized in a manual mode and are restored to an initial state point, the visual scene and a model can be initialized by clicking an initialization button or an accelerator switch, and the operation can be carried out in the flight process; the parameter receiving module is used for receiving an initialization instruction, a data recording updating instruction, a data playback instruction and a wind speed and direction simulating instruction input by an operation training person through the second intelligent interaction module, the maximum limit of the wind speed is 12m/s, and values of the wind speed and the wind direction can be changed on the accelerator stage. And the training evaluation unit also comprises a score evaluation module, and the flight operation data read by the score evaluation module is compared and judged according to a set scoring rule to obtain a training score.
The system also comprises a flight control unit, wherein the flight control unit comprises an accelerator stage and an operating lever, the accelerator stage comprises a vertical flight knob, a pause switch and a plurality of groups of control switches, the vertical flight knob and the pause switch are connected with the controller, after the visual scene is started and initialized, the pause switch is pushed to start the model clock, training personnel are controlled to vertically take off the airplane by rotating the vertical flight knob, when the height reaches the requirement, the vertical flight knob can be rotated to a zero position, and the plurality of groups of control switches comprise a model selection switch, a visual scene starting switch, an initialization switch, a subject selection switch, a data recording/ending recording switch, a data playback/ending playback switch and a manual/automatic switching switch. The system can switch automatic flight and manual flight, comprises a plurality of unmanned aerial vehicles, can realize vertical take-off and landing, can display longitude and latitude and height in a visual scene, and comprises a simulated unmanned aerial vehicle three-dimensional model and a three-dimensional simulation environment, and the visual angle can be switched between a first visual angle and a third visual angle.
As shown in fig. 5, in this embodiment, the performance evaluation process of the simulation training of the unmanned aerial vehicle includes: starting a system, carrying out communication connection, and selecting a model; clicking a starting view switch to start a corresponding switch; after the visual scene is started, clicking an initialization switch to initialize the system platform and the visual scene; pushing the "pause switch" (bringing the switch to the right position), starts the model clock; the vertical flight knob is rotated anticlockwise to enable the airplane to take off vertically, and when the height meets the requirement, the vertical flight knob can be rotated to a zero position (a blocking stop at the middle position); the throttle is pushed forward, so that the speed of the airplane can be increased, and the attitude of the airplane can be changed by rotating the rocker forward, backward, left and right; the switching between the automatic mode and the manual mode can be realized by clicking an automatic/manual button; and after the training is finished, recording and replaying data, reading the data, and comparing and judging the flight operation data according to a set grading rule to obtain a training score.
In this embodiment, the ground station control is based on the open source system Mission planer, which is suitable for fixed wing, rotorcraft and ground vehicle. The ground station control software may provide configuration tools or dynamic control to the automation device. The ground station control software and the FlightGear2018 simulation platform are built on the host, a complex open type flight simulator framework can be built, a real physical environment is generated and simulated, and flight control setting, air route planning, training mode selection and the like are carried out.
As shown in fig. 6, the ground station unit use method includes: after the hardware connection is finished, starting the simulation system and setting the simulation system to be in an automatic mode; starting a ground station host; after the start is finished, connecting the ground station with the simulation system, and after the connection is successful, starting the rocker to control and configure a flight plan, wherein the configured flight plan comprises configuration waypoint information, map route information and the like; setting a mode selection takeoff action, unlocking the airplane and starting flying operation; the automatic mode is selected after the takeoff is completed.
The configuration of the flight plan includes both simple and automatic route planning,
the simple route planning step comprises the following steps: firstly, selecting a necessary map, acquiring a plurality of waypoint position information on the necessary map, configuring specific waypoint commands such as taking off, landing, changing flight speed and controlling a camera to photograph and the like and proper heights for the plurality of waypoint position information, after the air route is planned, carrying out flight operation by the virtual unmanned aerial vehicle according to the air route planning, wherein the flying starting point has no coordinates and only has the height, and the flying starting point is a point where the aircraft is placed; the height of the landing point is 0, and the gyroplane LANDs by firstly flying to the LAND point coordinate with the current height and then starts to LAND after reaching the LAND coordinate.
The automatic route planning includes: drawing a polygon on the necessary map, framing a boundary range needing to fly, and selecting an automatic waypoint; setting parameters of flight tasks, overlapping degree and the like; after the setting is finished, at the starting point of the task acquired within the boundary range needing to fly, generating a corresponding air route task according to the setting parameters, and then starting the flying operation. For rotorcraft, it is desirable to modify the takeoff height to coincide with the course height. Wherein, the parameters for setting the flight mission comprise: and selecting parameters such as the model of the camera, the flying height, the flying speed and the like, and correspondingly changing the route preview generated by changing the parameters. Setting parameters such as overlapping degree comprises the following steps: the side direction overlapping degree is more than 70%, the course overlapping degree is related to the interval of the photographing distance, and the side direction overlapping degree can be determined according to the actual situation.
Fig. 7 is a visualization (third view angle) training interface of the present application under different simulated training scenarios, where "a" is a hill, "b" is a sea surface, "c" is a coast, "d" is a sky, and after clicking an initialization button, an initial state of the virtual drone is obtained. Fig. 8 is a data supervision interface in the training and evaluation process, and monitoring data curves of the virtual unmanned aerial vehicle, such as yaw angle, roll angle, course angle, height and the like, and fig. 9 is a visual control interface of the ground station of the present application, which shows a scene of the virtual unmanned aerial vehicle in flight operation control. In conclusion, the unmanned aerial vehicle simulation training system simulates a product machine model and an application scene, brings natural and real flight control experience to users, and provides a complete training solution from basic knowledge teaching to simulation training and operation scene practice for product users.
It should be noted that the described embodiments of the invention are only preferred ways of implementing the invention, and that all obvious modifications, which are within the scope of the invention, are all included in the present general inventive concept.
Claims (8)
1. An unmanned aerial vehicle simulated training system, comprising: the system comprises a three-dimensional simulation unit, a ground station unit and a training evaluation unit;
the three-dimensional simulation unit is used for carrying out flight simulation according to the unmanned aerial vehicle flight control data input by the ground station unit and displaying a route, a first visual angle, a third visual angle and a three-dimensional simulation environment on the intelligent display module;
the ground station unit is used for controlling training personnel to input flight control instructions and flight parameters and managing the sending states of the telemetering data, flight tracks and control instruction instructions;
the training evaluation unit is used for receiving flight parameters of the three-dimensional simulation unit virtual unmanned aerial vehicle through an intercommunicated network protocol, realizing flight training in different simulation environments according to set subjects and scene parameters, recording and playing back data of the flight training in different simulation environments, and reading training operation data to evaluate training operation scores.
2. The unmanned aerial vehicle simulation training system of claim 1, wherein the three-dimensional simulation unit comprises a simulation module, the simulation module receives a remote control command to change the flight attitude of the unmanned aerial vehicle, and establishes a mathematical model by using the pneumatic parameters, the wing section parameters and the power parameters of the aircraft according to a flight gear2018 platform to establish an equation and a control law of the aircraft, and simulates the flight attitude and the flight distance parameters of the aircraft by using time as a coordinate, and a flight control computer, a navigation computer, aircraft power, a pneumatic system and a steering engine device by using a mathematical simulation method.
3. The simulated training system of unmanned aerial vehicle of claim 2, wherein the three-dimensional simulation unit further comprises a data receiving module, the data receiving module is configured to receive input flight interaction commands and set parameters, the flight interaction commands comprise flight speed, attitude and altitude, and the set parameters comprise waypoint information and simulated environment parameter information.
4. The simulated training system of unmanned aerial vehicle of claim 3, wherein the ground station unit comprises a controller, an interface module, a control panel, a data transmission antenna, a host, and a charging module;
the control panel comprises a rocker module, a first intelligent interaction module and a plurality of groups of control buttons, the rocker module comprises a speed and direction control rocker and a flight attitude control rocker, the speed and direction control rocker is shifted up and down to control an accelerator, namely to control the speed, the left and right are shifted to control the direction, the flight attitude control rocker is shifted up and down to control the pitching of the airframe, the left and right are used for controlling the rolling of the airframe, the first intelligent interaction module is used for inputting flight control instructions, flight route planning instructions and displaying telemetering data, flight tracks and control instruction sending states, the first intelligent interaction module inputs the flight route planning instructions and comprises simple flight route planning and automatic flight route planning, the plurality of groups of control buttons comprise a power supply button, a starting button, a locking/unlocking button, a manual button, an automatic button, a self-defining button and a return flight button, the rocker module, the first intelligent interaction module and the plurality of groups of control buttons are all connected with the controller;
the interface module comprises an HDMI high-definition interface, a USB3.0 interface and a network interface, the interface module and the controller are both connected with the host, and the host is connected with the three-dimensional simulation unit and used for combining flight control parameters with the virtual unmanned aerial vehicle of the simulation module through an interface protocol;
the charging module is used for charging the ground station unit.
5. The simulated training system for unmanned aerial vehicles according to claim 4, wherein the ground station unit further comprises a power display module and a heat dissipation module, the power display module is used for displaying the remaining power of the ground command unit, the power display module comprises a power display, the heat dissipation module comprises a pair of heat dissipation fans, the pair of heat dissipation fans are electrically connected with the controller, and when the temperature of the system exceeds a set temperature threshold value, the controller controls the pair of heat dissipation fans to rotate for heat dissipation.
6. The unmanned aerial vehicle simulated training system of claim 5, wherein the training evaluation unit comprises a selection module, a switching module, a data management module, and a parameter receiving module;
the selection module is used for selecting different types and training subjects of the virtual unmanned aerial vehicle and starting the view of the corresponding type;
the switching module is used for switching between an automatic mode and a manual mode according to a state switching signal sent by the flight control unit, displaying the mode of the current state on a second intelligent interaction module of the console, and when the mode is in the manual mode, the model is driven by remote sensing data; when the model is in the automatic mode state, the model receives data sent by the ground station to drive the flight;
the data management module is used for recording and updating flight data, playing back the data and monitoring the flight data, and comprises a storage database, a recording control module, a data supervision module and an initialization module, wherein the storage database is used for storing the data in the model flight according to a storage list, the recording control module comprises a recording data/finishing recording button and a storage selection module, the recording data/finishing recording button is controlled, the system starts to record the flight data, at the moment, the training personnel is controlled to start operating the airplane flight, the recording data is required to be finished, the recording data/finishing recording button is controlled again, when the data is required to be stored, the training personnel is controlled to input the name of the data through the storage selection module to store the name, if the name is not input, the data is stored as a default data name, when the data do not need to be stored, the training personnel is controlled to select to cancel the storage through the storage selection module, the data supervision module is used for carrying out data playback according to a data playback instruction, deleting the recorded data according to a data deletion instruction, monitoring the yaw angle, the roll angle, the course angle and the height of the virtual unmanned aerial vehicle and indicating a data curve of the airspeed through the second intelligent interaction module, and the initialization module is used for initializing the data and the view;
the parameter receiving module is used for receiving an initialization instruction, a data recording updating instruction, a data playback instruction and an instruction for simulating wind speed and wind direction input by a training person through the second intelligent interaction module.
7. The simulated training system of unmanned aerial vehicle of claim 4, further comprising a flight control unit, the flight control unit is connected with the training evaluation unit and comprises a vertical flight knob, a pause switch, a control rod and a plurality of groups of control switches, the vertical flight knob and the pause switch are both connected with the controller, when the visual scene is started and the initialization is finished, the pause switch is pushed to start the model clock, the training personnel is controlled to vertically take off the airplane by rotating the vertical flight knob, when the height reaches the requirement, the vertical flying knob can be rotated to a zero position, and the multiple groups of control switches comprise a model selection switch, a scene starting switch, an initialization switch, a subject selection switch, a recorded data/end recording switch, a data playback/end playback switch and a manual/automatic switching switch.
8. The unmanned aerial vehicle simulation training system of claim 6, wherein the training evaluation unit further comprises a score evaluation module, and the flight operation data read by the score evaluation module is compared and judged according to a set scoring rule to obtain a training score.
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