Flight capability test platform

Abstract

The invention provides a flight capability test platform, and the platform comprises a flight simulation platform which is used for simulating a flight state according to flight data; the psychological quality evaluation device comprises a first detection unit, the first detection unit is used for detecting physiological signals, and the output end of the first detection unit is connected with the input end of the flight simulation platform; the physical fitness evaluation device comprises a pedal mechanism and a second detection unit, the pedal mechanism is used for providing pedal feedback, the second detection unit is used for detecting an action signal of the pedal mechanism, and the output end of the second detection unit is connected with the input end of the flight simulation platform. According to the flight ability test platform disclosed by the invention, psychological quality evaluation and physical quality evaluation of the system are introduced, so that a comprehensive flight ability evaluation system can be established, and a high-index selection demand is met.

Description

Technical Field

[0001] The present disclosure relates to the technical field of flight simulation, and in particular to a flight capability testing platform. Background Art

[0002] Since flight crews need to perform various special flight missions, they need extremely strong psychological and physical qualities. However, the current simulation test platform can only simulate simple flight conditions and cannot systematically evaluate the psychological and physical qualities of the subjects. It is not easy to form a comprehensive and integrated flight capability assessment system and it is difficult to meet the high selection requirements. Summary of the invention

[0003] The present disclosure aims to solve one of the technical problems in the related art at least to some extent.

[0004] To this end, an object of the present disclosure is to provide a flight capability test platform.

[0005] To achieve the above-mentioned purpose, the present disclosure provides a flight ability test platform, comprising: a flight simulation platform, which is used to simulate a flight state according to flight data; a psychological quality evaluation device, which is arranged on the flight simulation platform and comprises: a first detection unit, which is used to detect a physiological signal, and the output end of the first detection unit is connected to the input end of the flight simulation platform; a physical fitness evaluation device, which is arranged on the flight simulation platform and comprises: a pedal mechanism and a second detection unit, which is used to provide pedal feedback, and the second detection unit is used to detect an action signal of the pedal mechanism, and the output end of the second detection unit is connected to the input end of the flight simulation platform.

[0006] Optionally, the psychological quality assessment device also includes: a remaining ability testing unit, the remaining ability testing unit including: a plurality of test lights and a plurality of feedback buttons, the test lights and the feedback buttons are respectively arranged on the flight simulation platform, and the plurality of test lights and the plurality of feedback buttons correspond one to one; wherein, the input end of the test light is connected to the output end of the flight simulation platform, the output end of the feedback button is connected to the input end of the flight simulation platform, and the flight simulation platform is used to control at least one of the test lights to emit a test light, and record the delay time between the test light emitting the test light and the feedback button corresponding to the test light emitting a key signal.

[0007] Optionally, the psychological quality assessment device also includes: a stimulation unit, the stimulation unit includes: an electric stimulation vibration wristband, and the electric stimulation vibration wristband is used to electrically stimulate the wrist; wherein, the input end of the electric stimulation vibration wristband is connected to the output end of the flight simulation platform, and the flight simulation platform is used to control the electric stimulation vibration wristband to perform an electric stimulation action when the delay time exceeds a preset time.

[0008] Optionally, the first detection unit includes: a heart rate detection electrode, which is used to detect heart rate, and the output end of the heart rate detection electrode is connected to the input end of the flight simulation platform, wherein the flight simulation platform is used to record the heart rate in real time, and stop the flight simulation when the heart rate exceeds a preset heart rate range; and / or a skin resistance detection electrode, which is used to detect skin resistance, and the output end of the skin resistance detection electrode is connected to the input end of the flight simulation platform, wherein the flight simulation platform is used to record the skin resistance in real time, and stop the flight simulation when the skin resistance exceeds a preset skin resistance range; and / or a body temperature detection probe, which is used to detect body temperature, and the output end of the body temperature detection probe is connected to the input end of the flight simulation platform, wherein the flight simulation platform is used to record the body temperature in real time, and stop the flight simulation when the body temperature exceeds the preset body temperature range.

[0009] Optionally, the second detection unit includes: a weighing sensor, which is used to detect the pedal force applied to the pedal mechanism, and the output end of the weighing sensor is connected to the input end of the flight simulation platform, wherein the flight simulation platform is used to record the pedal force in real time, and simulate the flight state according to the pedal force and the flight data; and / or a first angular displacement sensor, which is used to detect the rudder deflection angle of the pedal mechanism under the action of the pedal force, and the output end of the first angular displacement sensor is connected to the input end of the flight simulation platform, wherein the flight simulation platform is used to record the rudder deflection angle in real time, and simulate the flight state according to the rudder deflection angle and the flight data; and / or a second angular displacement sensor, which is used to detect the pedal deflection angle of the pedal mechanism under the action of the pedal force, and the output end of the second angular displacement sensor is connected to the input end of the flight simulation platform, wherein the flight simulation platform is used to record the pedal deflection angle in real time, and simulate the flight state according to the pedal deflection angle and the flight data.

[0010] Optionally, the flight simulation platform includes: a cockpit, the cockpit including: a base, a front frame and a rear plate, the front frame and the rear plate are respectively arranged at two ends of the base, and the physical fitness assessment device is arranged at one end of the base close to the front frame, and the psychological fitness assessment device is arranged at one end of the base close to the rear plate; a seat, the seat is arranged at one end of the base close to the rear plate; a simulation unit, the simulation unit including: a host, a display and a control handle, the host and the display are respectively arranged on the front frame, and the display and the seat are arranged opposite to each other, the control handle is arranged on the seat, the input end of the host is respectively connected to the output end of the first detection unit, the output end of the second detection unit and the input end of the control handle, and the output end of the host is connected to the input end of the display.

[0011] Optionally, the flight simulation platform also includes: a shoulder pressure unit, which is arranged on the rear plate, and the shoulder pressure unit includes: a lifting plate, at least one shoulder pressure plate and a driving assembly, the lifting plate is slidably arranged on the rear plate, the shoulder pressure plate is arranged on the lifting plate, the driving assembly is transmission-connected to the lifting plate, and the driving assembly is used to drive the lifting plate to lift and lower so that the shoulder pressure plate is against or away from the shoulder.

[0012] Optionally, the driving assembly includes: a ball screw and at least one guide column, the ball screw is rotatably arranged on the rear plate, the guide column is arranged on the rear plate, the lifting plate is slidably arranged on the guide column, and the lifting plate is threadably connected to the ball screw; wherein the driving assembly also includes: a handwheel, the handwheel is transmission-connected to the ball screw, and the handwheel is used to drive the ball screw to rotate so as to lift the lifting plate; and / or a motor control module, a motor drive module and a shoulder press motor, the input end of the motor control module is connected to the output end of the host, and the output end of the motor control module is connected to the input end of the motor drive module, the output end of the motor drive module is connected to the input end of the shoulder press motor, the shoulder press motor is transmission-connected to the ball screw, and the shoulder press motor is used to drive the ball screw to rotate so as to lift the lifting plate.

[0013] Optionally, the shoulder pressure plate is rotatably arranged on the lifting plate, and a damper is arranged between the shoulder pressure plate and the lifting plate.

[0014] Optionally, the simulation unit also includes: an indicator light, which is arranged on the front frame and / or the rear panel, and the input end of the indicator light is connected to the output end of the host; and / or a speaker, which is arranged on the front frame and / or the rear panel, and the input end of the speaker is connected to the output end of the host; and / or a mouse, which is arranged on the front frame, and the output end of the mouse is connected to the input end of the host; and / or a keyboard, which is arranged on the front frame, and the output end of the keyboard is connected to the input end of the host.

[0015] The technical solution provided by the present disclosure may have the following beneficial effects:

[0016] Through the setting of the flight simulation platform, the trainees can use the flight simulation platform to realize the simulated training of the flight status, and through the setting of the first detection unit, the physiological reaction of the trainees can be detected, so as to facilitate the psychological quality assessment of the trainees according to the physiological reaction of the trainees, and at the same time, through the setting of the pedal mechanism and the second detection unit, the pedal feedback and the detection of the pedaling action of the trainees can be realized, so as to facilitate the physical quality assessment of the trainees according to the pedaling action of the trainees; therefore, the psychological quality assessment device and the physical quality assessment device are set on the flight simulation platform, which can introduce the systematic psychological quality assessment and physical quality assessment while the trainees are simulating the training flight status, so as to facilitate the establishment of a comprehensive and integrated flight ability assessment system, thereby meeting the high-index selection needs.

[0017] Additional aspects and advantages of the present disclosure will be given in part in the following description and in part will be obvious from the following description or learned through practice of the present disclosure. BRIEF DESCRIPTION OF THE DRAWINGS

[0018] The above and / or additional aspects and advantages of the present disclosure will become apparent and easily understood from the following description of the embodiments in conjunction with the accompanying drawings, in which:

[0019] Figure 1 is a structural schematic diagram of a flight capability test platform proposed in an embodiment of the present disclosure;

[0020] Figure 2 is a structural schematic diagram of a flight capability test platform proposed in an embodiment of the present disclosure;

[0021] Figure 3 is a circuit diagram of a flight capability test platform proposed in an embodiment of the present disclosure;

[0022] Figure 4 is a circuit diagram of a flight capability test platform proposed in an embodiment of the present disclosure;

[0023] Figure 5 is a circuit diagram of a flight capability test platform proposed in an embodiment of the present disclosure;

[0024] Figure 6 It is a structural schematic diagram of a shoulder pressing unit in a flight capability test platform proposed in an embodiment of the present disclosure;

[0025] As shown in the figure: 1. Flight simulation platform;

[0026] 11. cockpit, 111. base, 112. front frame, 113. rear plate;

[0027] 12. Seats;

[0028] 13. simulation unit, 131. host, 132. display, 133. control handle, 134. indicator light, 135. speaker, 136. mouse, 137. keyboard;

[0029] 14. Shoulder press unit, 141. Lifting plate, 142. Shoulder press plate, 143. Ball screw, 144. Guide column, 145. Hand wheel, 146. Motor control module, 147. Motor drive module, 148. Shoulder press motor;

[0030] 2. Psychological quality assessment device;

[0031] 21. a first detection unit, 211. a heart rate detection electrode, 212. a skin resistance detection electrode, 213. a body temperature detection probe;

[0032] 22. Remaining capacity test unit, 221. Test light, 222. Feedback button;

[0033] 23. Stimulation unit, 231. Electrical stimulation vibration wristband;

[0034] 3. Physical fitness assessment device;

[0035] 31. Pedal mechanism;

[0036] 32. A second detection unit, 321. A weighing sensor, 322. A first angular displacement sensor, 323. A second angular displacement sensor. DETAILED DESCRIPTION

[0037] Embodiments of the present disclosure are described in detail below, examples of which are shown in the accompanying drawings, wherein the same or similar reference numerals throughout represent the same or similar elements or elements having the same or similar functions. The embodiments described below with reference to the accompanying drawings are exemplary and are only used to explain the present disclosure, and are not to be construed as limitations of the present disclosure. On the contrary, the embodiments of the present disclosure include all changes, modifications, and equivalents that fall within the spirit and connotation of the appended claims.

[0038] like Figure 1 and Figure 3 As shown, the embodiment of the present disclosure proposes a flight ability test platform, including: a flight simulation platform 1, a psychological quality evaluation device 2 and a physical quality evaluation device 3, the flight simulation platform 1 is used to simulate the flight state according to the flight data, the psychological quality evaluation device 2 is arranged on the flight simulation platform 1, and the psychological quality evaluation device 2 includes: a first detection unit 21, the first detection unit 21 is used to detect physiological signals, and the output end of the first detection unit 21 is connected to the input end of the flight simulation platform 1, the physical quality evaluation device 3 is arranged on the flight simulation platform 1, and the physical quality evaluation device 3 includes: a pedal mechanism 31 and a second detection unit 32, the pedal mechanism 31 is used to provide pedal feedback, the second detection unit 32 is used to detect the action signal of the pedal mechanism 31, and the output end of the second detection unit 32 is connected to the input end of the flight simulation platform 1.

[0039] It can be understood that, through the setting of the flight simulation platform 1, the trainees can use the flight simulation platform 1 to realize simulated training of the flight state, and, through the setting of the first detection unit 21, the physiological reaction of the trainees can be detected, so as to facilitate the psychological quality assessment of the trainees according to the physiological reaction of the trainees, and at the same time, through the setting of the pedal mechanism 31 and the second detection unit 32, pedal feedback and detection of the trainees' pedaling movements can be realized, so as to facilitate the physical fitness assessment of the trainees according to the trainees' pedaling movements.

[0040] Therefore, by setting up the psychological quality assessment device 2 and the physical fitness assessment device 3 on the flight simulation platform 1, it is possible to introduce systematic psychological quality assessment and physical fitness assessment while the trainees are simulating the training flight state, thereby facilitating the establishment of a comprehensive and integrated flight ability assessment system, thereby meeting the high-index selection requirements.

[0041] It should be noted that the flight simulation platform 1 is used to simulate the flight status based on the flight data. For example, a tracking flight mission is set according to the real flight data, so that trainees can simulate the flight status with the help of the tracking flight mission. The specific type of the flight simulation platform 1 can be set according to actual needs and there is no restriction on this.

[0042] The psychological quality assessment device 2 is used to assess the psychological quality of trainees. The first detection unit 21 in the psychological quality assessment device 2 is used to detect the physiological signals of the trainees, for example: judging the emotional stability, stress tolerance, etc. of the trainees in various scenarios based on the physiological signals. The specific type of the first detection unit 21 can be set according to actual needs and is not limited to this.

[0043] The physical fitness assessment device 3 is used to assess the physical fitness of trainees. The pedal mechanism 31 in the physical fitness assessment device 3 is used to provide pedal feedback, so as to utilize pedal feedback to achieve real simulated flight training, independent physical fitness assessment, etc. The pedal feedback second detection unit 32 is used to detect the action signal of the pedal mechanism 31, for example: detecting the pedal force signal, rudder angle signal, pedal angle signal, etc. generated after the trainees apply force on the pedal mechanism 31. The specific types of the pedal mechanism 31 and the second detection unit 32 can be set according to actual needs and are not limited to this.

[0044] For example, the pedal mechanism 31 may include a bracket, a rudder frame and a pedal, the rudder frame is rotatably arranged on the bracket, the pedal is rotatably arranged on the rudder frame, and the pedal mechanism 31 may adopt a CLJD-2A type force-measuring pedal, which can simulate the normal operation of the rudder and realize the anti-overload pedal force training. Among them, the first detection unit 21 detects the pressure on the pedal to obtain the pedal force, the first detection unit 21 detects the rotation angle of the rudder frame to obtain the rudder deflection angle, and the first detection unit 21 detects the rotation angle of the pedal to obtain the pedal angle; a damping piston cylinder may be arranged between the rudder frame and the bracket and between the pedal and the rudder frame to provide pedal feedback by using the damping piston cylinder; the bracket may be arranged as a three-dimensional motion structure to realize the adjustment of the pedal position under the control of the flight simulation platform 1, so as to adapt to different trainees.

[0045] like Figure 1 , Figure 3 and Figure 4 As shown, in some embodiments, the psychological quality evaluation device 2 further includes: a residual ability test unit 22, the residual ability test unit 22 includes: a plurality of test lights 221 and a plurality of feedback buttons 222, the test lights 221 and the feedback buttons 222 are respectively arranged on the flight simulation platform 1, and the plurality of test lights 221 and the plurality of feedback buttons 222 correspond to each other. Among them, the input end of the test light 221 is connected to the output end of the flight simulation platform 1, the output end of the feedback button 222 is connected to the input end of the flight simulation platform 1, and the flight simulation platform 1 is used to control at least one test light 221 to emit a test light 221 light, and record the delay time between the test light 221 emitting the test light 221 light and the feedback button 222 corresponding to the test light 221 emitting a key signal.

[0046] It can be understood that since the input end of the test light 221 is connected to the output end of the flight simulation platform 1, and the output end of the feedback button 222 is connected to the input end of the flight simulation platform 1, the flight simulation platform 1 can control the test light 221 to emit the test light 221 light, and at the same time can receive the key signal emitted by the feedback button 222. Therefore, by comparing the time when the test light 221 emits the test light 221 light and the time when the feedback button 222 emits the key signal, the reaction delay time of the trainee can be obtained, thereby facilitating the testing of the trainee's remaining ability, and further facilitating the establishment of a comprehensive and integrated flight ability evaluation system.

[0047] It should be noted that the residual capacity test refers to determining whether the trainee has residual energy to complete other test items while performing flight mission simulation and other actions, such as a light test with the cooperation of multiple test lights 221 and multiple feedback buttons 222. Among them, by using the cooperation of multiple test lights 221 and multiple feedback buttons 222 in the residual capacity test unit 22, it is possible to determine whether the trainee's button press is correct according to the corresponding test lights 221 and feedback buttons 222, and the trainee's reaction speed can be calculated according to the reaction delay time.

[0048] The test light 221 is used to emit a test light 221 light, for example, emitting a light of a corresponding color, emitting a light flashing at a corresponding frequency, etc. The specific type of the test light 221 can be set according to actual needs and is not limited to this.

[0049] The feedback button 222 is used to send a button signal. The specific type of the feedback button 222 can be set according to actual needs and is not limited to this.

[0050] Among them, the number of test lights 221 and feedback buttons 222 can be set according to actual needs, and there is no limitation on this. For example, the number of test lights 221 and feedback buttons 222 can be nine respectively, that is, a nine-light remaining capacity test.

[0051] like Figure 3 and Figure 4 As shown, in some embodiments, the psychological quality assessment device 2 further includes: a stimulation unit 23, the stimulation unit 23 includes: an electric stimulation vibration wristband 231, and the electric stimulation vibration wristband 231 is used to electrically stimulate the wrist. Among them, the input end of the electric stimulation vibration wristband 231 is connected to the output end of the flight simulation platform 1, and the flight simulation platform 1 is used to control the electric stimulation vibration wristband 231 to perform an electric stimulation action when the delay time exceeds the preset time.

[0052] It can be understood that since the input end of the electric stimulation vibration wristband 231 is connected to the output end of the flight simulation platform 1, the flight simulation platform 1 can use the electric stimulation vibration wristband 231 to emit electric stimulation to the trainee's wrist, thereby playing a role in reminding the trainee, for example: when the delay time exceeds the preset time, the electric stimulation vibration wristband 231 is controlled to perform the electric stimulation action, thereby reminding the trainee to conduct the remaining ability test in time; at the same time, the electric stimulation vibration wristband 231 is used to emit electric stimulation to the trainee's wrist, and it can also cooperate with the first detection unit 21 to enable the trainee to conduct emotional stability and stress tolerance test evaluation, which is conducive to the establishment of a comprehensive and integrated flight ability evaluation system.

[0053] It should be noted that sending electrical stimulation to the trainee's wrist can not only remind the trainee to perform the corresponding test actions in time, but also can test the trainee's psychological quality.

[0054] For example, after the track tracking task begins, when the circular sight controlled by the subject enters 60-80 distance units from the target aircraft, wrist vibration interference is applied to the subject.

[0055] The electrical stimulation vibration wristband 231 is used for electrical stimulation of the wrist. The specific type of the electrical stimulation vibration wristband 231 can be set according to actual needs and is not limited to this.

[0056] The preset time can be set according to actual needs and there is no limitation on this. For example, the preset time can be 2s, that is, when the delay time exceeds 2s, the electric stimulation vibration wristband 231 is controlled to perform the electric stimulation action, and the stimulation is continued for 2s every 2s until the trainee makes a corresponding action.

[0057] like Figure 4 As shown, in some embodiments, the first detection unit 21 includes: a heart rate detection electrode 211, the heart rate detection electrode 211 is used to detect the heart rate, and the output end of the heart rate detection electrode 211 is connected to the input end of the flight simulation platform 1, wherein the flight simulation platform 1 is used to record the heart rate in real time, and stop the flight simulation when the heart rate exceeds a preset heart rate range.

[0058] It can be understood that since the output end of the heart rate detection electrode 211 is connected to the input end of the flight simulation platform 1, the heart rate detection electrode 211 can send the detected heart rate of the trainee to the flight simulation platform 1, so that the flight simulation platform 1 can evaluate the psychological quality of the trainees according to their heart rate, thereby realizing a comprehensive and integrated flight ability assessment of the trainees.

[0059] It should be noted that the heart rate detection electrode 211 is used to detect the heart rate of the trainee, and the specific type of the heart rate detection electrode 211 can be set according to actual needs and is not limited to this.

[0060] Before the flight simulation begins or during the flight simulation, if the trainee's heart rate exceeds a preset heart rate range, the flight simulation is stopped to protect the trainee and avoid problems such as incorrect wearing of the heart rate detection electrode 211.

[0061] At the same time, the trainee's heart rate detected by the heart rate detection electrode 211 can be used to determine the trainee's emotional stability and stress tolerance, thereby achieving a psychological quality assessment of the trainee.

[0062] like Figure 4 As shown, in some embodiments, the first detection unit 21 includes: a skin resistance detection electrode 212, the skin resistance detection electrode 212 is used to detect skin resistance, and the output end of the skin resistance detection electrode 212 is connected to the input end of the flight simulation platform 1, wherein the flight simulation platform 1 is used to record the skin resistance in real time, and stop the flight simulation when the skin resistance exceeds a preset skin resistance range.

[0063] It can be understood that since the output end of the skin resistance detection electrode 212 is connected to the input end of the flight simulation platform 1, the skin resistance detection electrode 212 can send the detected skin resistance of the trainee to the flight simulation platform 1, so that the flight simulation platform 1 can evaluate the psychological quality of the trainees according to the skin resistance of the trainees, and further realize a comprehensive and integrated flight ability assessment of the trainees.

[0064] It should be noted that the skin resistance detection electrode 212 is used to detect the skin resistance of the trainee, and the specific type of the skin resistance detection electrode 212 can be set according to actual needs and is not limited to this.

[0065] Before the flight simulation begins or during the flight simulation, if the trainee's skin resistance exceeds a preset skin resistance range, the flight simulation is stopped to protect the trainee and avoid problems such as incorrect wearing of the skin resistance detection electrode 212.

[0066] At the same time, the trainee's skin resistance detected by the skin resistance detection electrode 212 can be used to determine the trainee's emotional stability and stress tolerance, thereby achieving a psychological quality assessment of the trainee. Specifically, if the trainee is nervous and sweats, the skin resistance will decrease.

[0067] like Figure 4As shown, in some embodiments, the first detection unit 21 includes: a body temperature detection probe 213, the body temperature detection probe 213 is used to detect body temperature, and the output end of the body temperature detection probe 213 is connected to the input end of the flight simulation platform 1, wherein the flight simulation platform 1 is used to record body temperature in real time, and stop the flight simulation when the body temperature exceeds a preset body temperature range.

[0068] It can be understood that since the output end of the temperature detection probe 213 is connected to the input end of the flight simulation platform 1, the temperature detection probe 213 can send the detected body temperature of the trainee to the flight simulation platform 1, so that the flight simulation platform 1 can evaluate the psychological quality of the trainees based on their body temperature, thereby achieving a comprehensive and integrated flight ability assessment of the trainees.

[0069] It should be noted that the body temperature detection probe 213 is used to detect the body temperature of the trainee, and the specific type of the body temperature detection probe 213 can be set according to actual needs and is not limited to this.

[0070] Before the flight simulation begins or during the flight simulation, if the trainee's body temperature exceeds the preset temperature range, the flight simulation is stopped to protect the trainee and avoid problems such as incorrect wearing of the temperature detection probe 213.

[0071] At the same time, the trainee's body temperature detected by the body temperature detection probe 213 can be used to determine the trainee's emotional stability and stress tolerance, thereby achieving a psychological quality assessment of the trainee.

[0072] like Figure 4 As shown, in some embodiments, the second detection unit 32 includes: a weighing sensor 321, the weighing sensor 321 is used to detect the pedal force applied to the pedal mechanism 31, and the output end of the weighing sensor 321 is connected to the input end of the flight simulation platform 1, wherein the flight simulation platform 1 is used to record the pedal force in real time, and simulate the flight state according to the pedal force and flight data;

[0073] It can be understood that since the output end of the weighing sensor 321 is connected to the input end of the flight simulation platform 1, the weighing sensor 321 can send the pedal force applied to the pedal mechanism 31 to the flight simulation platform 1, so that the flight simulation platform 1 can evaluate the physical fitness based on the pedal force, thereby realizing a comprehensive and integrated flight ability assessment of the trainees.

[0074] It should be noted that the weighing sensor 321 is used to detect the pedal force applied to the pedal mechanism 31 , and the specific type of the weighing sensor 321 can be set according to actual needs, and there is no limitation on this.

[0075] The pedaling force detected by the weighing sensor 321 can be used to determine the physical fitness of the trainee, thereby realizing the physical fitness evaluation of the trainee.

[0076] like Figure 4 As shown, in some embodiments, the second detection unit 32 includes: a first angular displacement sensor 322, the first angular displacement sensor 322 is used to detect the rudder deflection angle of the pedal mechanism 31 under the pedal force, and the output end of the first angular displacement sensor 322 is connected to the input end of the flight simulation platform 1, wherein the flight simulation platform 1 is used to record the rudder deflection angle in real time, and simulate the flight state according to the rudder deflection angle and the flight data;

[0077] It can be understood that since the output end of the first angular displacement sensor 322 is connected to the input end of the flight simulation platform 1, the first angular displacement sensor 322 can send the detected rudder deflection angle of the pedal mechanism 31 under the action of the pedal force to the flight simulation platform 1, so that the flight simulation platform 1 can evaluate the physical fitness according to the rudder deflection angle, and thus achieve a comprehensive and integrated flight ability assessment of the trainees.

[0078] It should be noted that the first angular displacement sensor 322 is used to detect the rudder deflection angle of the pedal mechanism 31 under the pedal force, and the specific type of the first angular displacement sensor 322 can be set according to actual needs and is not limited to this. Among them, the first angular displacement sensor 322 can be set between the bracket of the pedal mechanism 31 and the rudder frame.

[0079] The rudder deflection angle detected by the first angular displacement sensor 322 can be used to determine the pedal control ability of the trainee, thereby achieving physical fitness assessment of the trainee.

[0080] like Figure 4 As shown, in some embodiments, the second detection unit 32 includes: a second angular displacement sensor 323, the second angular displacement sensor 323 is used to detect the pedal deflection angle of the pedal mechanism 31 under the action of the pedal force, and the output end of the second angular displacement sensor 323 is connected to the input end of the flight simulation platform 1, wherein the flight simulation platform 1 is used to record the pedal deflection angle in real time, and simulate the flight state according to the pedal deflection angle and flight data.

[0081] It can be understood that since the output end of the second angular displacement sensor 323 is connected to the input end of the flight simulation platform 1, the second angular displacement sensor 323 can send the detected pedal deflection angle of the pedal mechanism 31 under the action of the pedal force to the flight simulation platform 1, so that the flight simulation platform 1 can evaluate the physical fitness according to the pedal deflection angle, and thus achieve a comprehensive and integrated flight ability assessment of the trainees.

[0082] It should be noted that the second angular displacement sensor 323 is used to detect the pedal deflection angle of the pedal mechanism 31 under the pedal force, and the specific type of the second angular displacement sensor 323 can be set according to actual needs and is not limited to this. Among them, the second angular displacement sensor 323 can be set between the pedal of the pedal mechanism 31 and the steering frame.

[0083] The pedal deflection angle detected by the second angular displacement sensor 323 can be used to determine the trainee's pedal control ability, thereby achieving a physical fitness assessment of the trainee.

[0084] At the same time, according to the pedal force detected by the weighing sensor 321, the rudder angle detected by the first angular displacement sensor 322, and the pedal angle detected by the second angular displacement sensor 323, a more realistic flight simulation can be achieved.

[0085] like Figure 1 , Figure 2 , Figure 3 , Figure 4 and Figure 5 As shown, in some embodiments, the flight simulation platform 1 includes: a cockpit 11, a seat 12 and a simulation unit 13, the cockpit 11 includes: a base 111, a front frame 112 and a rear plate 113, the front frame 112 and the rear plate 113 are respectively arranged at both ends of the base 111, and the physical fitness evaluation device 3 is arranged at one end of the base 111 close to the front frame 112, the psychological quality evaluation device 2 is arranged at one end of the base 111 close to the rear plate 113, and the seat 12 is arranged at one end of the base 111 close to the rear plate 113, the simulation unit 13 includes: a host 131, a display 132 and a control handle 133, the host 131 and the display 132 are respectively arranged on the front frame 112, and the display 132 and the seat 12 are arranged opposite to each other, the control handle 133 is arranged on the seat 12, the input end of the host 131 is respectively connected to the output end of the first detection unit 21, the output end of the second detection unit 32 and the input end of the control handle 133, and the output end of the host 131 is connected to the input end of the display 132.

[0086] It can be understood that since the input end of the host 131 is respectively connected to the output end of the first detection unit 21, the output end of the second detection unit 32 and the input end of the control handle 133, and the output end of the host 131 is connected to the input end of the display 132, the trainees can use the processing control of the host 131, the control of the control handle 133 and the display of the display 132 to achieve a more realistic flight simulation, as well as a stable assessment of the psychological and physical qualities, thereby achieving a comprehensive and integrated flight ability assessment of the trainees.

[0087] It should be noted that the cockpit 11 is used to carry components such as the seat 12, the psychological quality assessment device 2, the physical quality assessment device 3, and the simulation unit 13. The specific type of the cockpit 11 can be set according to actual needs and is not limited to this. For example, the base 111, the front frame 112, and the rear plate 113 constitute a cockpit 11 structure that is close to a U-shaped structure. Among them, multiple test lights 221 can be set on the front frame 112, and the multiple test lights 221 and the seat 12 are arranged relative to each other.

[0088] The seat 12 is used to provide seats for trainees to simulate real flight conditions. The specific type of the seat 12 can be set according to actual needs and is not limited to this. For example, the seat 12 has components such as a seat, armrests, and a backrest.

[0089] The host 131 is used for signal output, input, and calculation processing, etc. The specific type of the host 131 can be set according to actual needs and is not limited to this. In particular, in order to cooperate with the test light 221, the electrical stimulation vibration wristband 231, the heart rate detection electrode 211 and other devices, the host 131 can also be configured with a conversion circuit board and a converter for signal conversion; the host 131 processes and comprehensively analyzes the real-time sampling and data recording during the simulation training and evaluation process, and then saves the test process data and the evaluation result data to the database, and displays the evaluation results on the display 132 and feeds back to the trainees.

[0090] Among them, regarding the use of the database:

[0091] 1. Data browsing: This function use case is mainly provided for the main test personnel to browse and view the original data records, evaluation indicators and corresponding scores of the trainees who have completed the test. Specifically, click the "Database" button in the main interface to enter the data browsing interface, which gives the basic information of the trainees in the form of a list. After double-clicking one of the personnel records with the mouse 136, the completed test record information and evaluation indicator data will be displayed in another list. After double-clicking a test record data in the list, the real-time sampled heart rate and pedaling force data will be displayed in a waveform chart, and the original data of the tracking error and the nine-light remaining capacity reaction record data will be given in text form. This function use case is also the leading use case of the database management and data export use cases.

[0092] 2. Database management and data export: This function case is mainly provided to the test personnel to perform database management related operations such as database backup, recovery, and clearing, and can realize the export of original data and evaluation result data in the existing database to Excel tables for subsequent processing such as statistics, summary, and printing. The target software system data training temporarily uses MS Office Access database for data storage.

[0093] The display 132 is used to display the flight simulation screen and the data parameters detected by the psychological quality evaluation device 2, the physical quality evaluation device 3, etc. The specific type of the display 132 can be set according to actual needs and there is no limitation on this. For example, the display 132 uses a 34-inch curved high-resolution Samsung display 132.

[0094] Among them, the data parameters displayed on the display 132 may include: waveform graphs of real-time physiological signals (heart rate, pedaling force, etc.), bar charts, scrolling refresh of text, presentation of track tracking tasks, corresponding display of the test light 221 and the feedback button 222 in the remaining capacity test, etc.

[0095] The control handle 133 is used by trainees to input control instructions to the host 131. The specific type of the control handle 133 can be set according to actual needs and is not limited to this. For example, the control handle 133 includes: a joystick and a throttle lever, and multiple feedback buttons 222 can be set on the throttle lever.

[0096] like Figure 2 , Figure 3 and Figure 4 As shown, in some embodiments, the flight simulation platform 1 also includes: a shoulder pressure unit 14, which is arranged on the rear plate 113, and the shoulder pressure unit 14 includes: a lifting plate 141, at least one shoulder pressure plate 142 and a driving assembly, the lifting plate 141 is slidably arranged on the rear plate 113, the shoulder pressure plate 142 is arranged on the lifting plate 141, the driving assembly is transmission-connected to the lifting plate 141, and the driving assembly is used to drive the lifting plate 141 to lift and lower so that the shoulder pressure plate 142 is against or away from the shoulder.

[0097] It can be understood that, by providing the shoulder pressure plate 142, the flight simulation of the trainees can be made more realistic, thereby ensuring the stable assessment of the trainees. At the same time, since the driving component and the lifting plate 141 are connected by transmission, the driving component can drive the lifting plate 141 to rise and fall, thereby realizing that the shoulder pressure plate 142 is against or away from the shoulder, thereby making the use of the shoulder pressure plate 142 more flexible and convenient.

[0098] It should be noted that the lifting plate 141 is used to support the shoulder plate 142 , and the specific type of the lifting plate 141 can be set according to actual needs, and there is no limitation on this.

[0099] The shoulder pressure plate 142 is used to rest against the trainee's shoulders to make the trainee's flight simulation more stable and realistic. The specific type of the shoulder pressure plate 142 can be set according to actual needs and is not limited to this. For example, the shoulder pressure plate 142 is a long strip plate structure, and two shoulder pressure plates 142 are provided, and the two shoulder pressure plates 142 correspond to the two shoulders of the trainee.

[0100] The driving component is used to drive the lifting plate 141 to move up and down. The specific type of the driving component can be set according to actual needs and is not limited to this.

[0101] like Figure 5 and Figure 6 As shown, in some embodiments, the driving assembly includes: a ball screw 143 and at least one guide column 144, the ball screw 143 is rotatably set on the rear plate 113, the guide column 144 is set on the rear plate 113, the lifting plate 141 is slidably set on the guide column 144, and the lifting plate 141 and the ball screw 143 are connected by threaded transmission.

[0102] Among them, the driving component also includes: a handwheel 145, which is connected to the ball screw 143 by transmission, and the handwheel 145 is used to drive the ball screw 143 to rotate so that the lifting plate 141 can be lifted and lowered; and / or, the driving component also includes: a motor control module 146, a motor drive module 147 and a shoulder press motor 148, the input end of the motor control module 146 is connected to the output end of the host 131, and the output end of the motor control module 146 is connected to the input end of the motor drive module 147, the output end of the motor drive module 147 is connected to the input end of the shoulder press motor 148, the shoulder press motor 148 is connected to the ball screw 143 by transmission, and the shoulder press motor 148 is used to drive the ball screw 143 to rotate so that the lifting plate 141 can be lifted and lowered.

[0103] It can be understood that since the lifting plate 141 is slidably set on the guide column 144, the lifting plate 141 can slide on the rear plate 113 by means of the guide column 144, and since the lifting plate 141 and the ball screw 143 are connected by threaded transmission, the ball screw 143 can use rotation to drive the lifting plate 141 to rise and fall on the rear plate 113.

[0104] Therefore, since the handwheel 145 and the ball screw 143 are connected in transmission, the handwheel 145 can drive the ball screw 143 to rotate, thereby realizing manual lifting of the lifting plate 141, and then realizing the shoulder pressure plate 142 to abut against or move away from the shoulder; since the shoulder pressure motor 148 and the ball screw 143 are connected in transmission, the shoulder pressure motor 148 can drive the ball screw 143 to rotate under the control of the motor control module 146 and the motor drive module 147, thereby realizing automatic lifting of the lifting plate 141, and then realizing the shoulder pressure plate 142 to abut against or move away from the shoulder.

[0105] It should be noted that the guide column 144 is used to guide the lifting plate 141 . The specific type of the guide column 144 can be set according to actual needs and is not limited to this. For example, the guide column 144 is a smooth columnar structure, and a corresponding column sleeve is provided on the lifting plate 141 .

[0106] The ball screw 143 is used to drive the lifting plate 141 . The specific type of the ball screw 143 can be set according to actual needs and is not limited thereto.

[0107] The hand wheel 145 is used to manually drive the ball screw 143 to rotate. The specific type of the hand wheel 145 can be set according to actual needs and is not limited to this. Wherein, the hand wheel 145 can be located at the top of the rear plate 113.

[0108] The motor control module 146 is used to control the motor drive module 147 according to the command of the host 131. The specific type of the motor control module 146 can be set according to actual needs and is not limited to this. For example, the motor control module 146 can be a controller.

[0109] The motor driving module 147 is used to drive the shoulder pressing motor 148 to control the forward and reverse rotation and speed of the shoulder pressing motor 148, thereby realizing the reciprocating linear motion of the shoulder pressing plate 142. The specific type of the motor driving module 147 can be set according to actual needs and is not limited to this. For example, the motor driving module 147 can be a driver.

[0110] The shoulder press motor 148 is used to automatically drive the ball screw 143 to rotate. The specific type of the shoulder press motor 148 can be set according to actual needs and is not limited to this. For example, the shoulder press motor 148 can be a stepper motor, which is an open-loop control element that converts an electrical pulse signal into angular displacement or linear displacement.

[0111] In some embodiments, the shoulder pressing plate 142 is rotatably disposed on the lifting plate 141 , and a damper is disposed between the shoulder pressing plate 142 and the lifting plate 141 .

[0112] It can be understood that since the shoulder plate 142 is rotatably set on the lifting plate 141, and a damper is provided between the shoulder plate 142 and the lifting plate 141, the shoulder plate 142 can adjust its angle according to actual needs, thereby adapting to different trainees and being more flexible and convenient to use.

[0113] It should be noted that the damper is used to provide damping force for the shoulder plate 142, and the damping force should be greater than the sagging force generated by the shoulder plate 142 due to its own weight, so as to ensure that the shoulder plate 142 can be positioned after the angle is adjusted. The specific type of the damper can be set according to actual needs and is not limited to this.

[0114] like Figure 1 , Figure 2 and Figure 5 As shown, in some embodiments, the simulation unit 13 further includes: an indicator light 134, the indicator light 134 is arranged on the front frame 112 and / or the rear plate 113, and the input end of the indicator light 134 is connected to the output end of the host 131;

[0115] It can be understood that since the indicator light 134 is set on the front frame 112 and / or the rear panel 113, and the input end of the indicator light 134 is connected to the output end of the host 131, the host 131 can use the indicator light 134 to achieve an indication function, thereby making the use of the flight simulation platform 1 more flexible and convenient.

[0116] It should be noted that the indicator light 134 is used to emit light. The specific type of the indicator light 134 can be set according to actual needs and is not limited to this. For example, the indicator light 134 can be an acrylic lamp, and the indicator light 134 is set on the side of the front frame 112.

[0117] like Figure 5 As shown, in some embodiments, the simulation unit 13 further includes: a speaker 135 , the speaker 135 is disposed on the front frame 112 and / or the rear panel 113 , and an input end of the speaker 135 is connected to an output end of the host 131 .

[0118] It can be understood that since the speaker 135 is arranged on the front frame 112 and / or the rear panel 113, and the input end of the speaker 135 is connected to the output end of the host 131, the host 131 can use the speaker 135 to achieve sound simulation and indication, thereby making the use of the flight simulation platform 1 more flexible and convenient.

[0119] It should be noted that the speaker 135 is used to make sounds, and the specific type of the speaker 135 can be set according to actual needs and is not limited to this.

[0120] like Figure 5 As shown, in some embodiments, the simulation unit 13 further includes: a mouse 136 , which is disposed on the front frame 112 , and an output end of the mouse 136 is connected to an input end of the host 131 .

[0121] It is understandable that, since the mouse 136 is arranged on the front frame 112 and the output end of the mouse 136 is connected to the input end of the host 131, the host 131 can use the mouse 136 to receive external control instructions, thereby making the use of the flight simulation platform 1 more flexible and convenient.

[0122] It should be noted that the mouse 136 is used to output control instructions to the host 131, and the specific type of the mouse 136 can be set according to actual needs and is not limited to this.

[0123] like Figure 5 As shown, in some embodiments, the simulation unit 13 further includes: a keyboard 137 , the keyboard 137 is disposed on the front frame 112 , and an output end of the keyboard 137 is connected to an input end of the host 131 .

[0124] It can be understood that since the keyboard 137 is set on the front frame 112, and the output end of the keyboard 137 is connected to the input end of the host 131, the host 131 can use the keyboard 137 to receive external control instructions, thereby making the use of the flight simulation platform 1 more flexible and convenient.

[0125] It should be noted that the keyboard 137 is used to output control instructions to the host 131, and the specific type of the keyboard 137 can be set according to actual needs and is not limited to this.

[0126] Among them, the flight simulation platform 1 can be integrated as a whole through the assembly of six parts. Specifically, the assembly of the six parts includes: base 111 assembly, front frame 112 assembly, display 132 frame assembly, shoulder pressure unit 14 assembly, acrylic light panel assembly, seat 12 and rear panel 113 assembly.

[0127] The flight capability test platform also includes a power module, which is used to provide stable electrical energy to various electrical components.

[0128] In the description of the present disclosure, the terms "first", "second", etc. are used for descriptive purposes only and cannot be understood as indicating or implying relative importance. In addition, in the description of the present disclosure, unless otherwise specified, "plurality" means two or more.

[0129] Any process or method description in a flowchart or otherwise described herein may be understood to represent a module, segment or portion of code that includes one or more executable instructions for implementing the steps of a specific logical function or process, and the scope of the preferred embodiments of the present disclosure includes alternative implementations in which functions may not be performed in the order shown or discussed, including performing functions in a substantially simultaneous manner or in the reverse order depending on the functions involved, which should be understood by those skilled in the art to which the embodiments of the present disclosure belong.

[0130] In the description of this specification, the description with reference to the terms "one embodiment", "some embodiments", "example", "specific example", or "some examples" means that the specific features, structures, materials or characteristics described in conjunction with the embodiment or example are included in at least one embodiment or example of the present disclosure. In this specification, the schematic representation of the above terms does not necessarily refer to the same embodiment or example. Moreover, the specific features, structures, materials or characteristics described may be combined in any one or more embodiments or examples in a suitable manner.

[0131] Although the embodiments of the present disclosure have been shown and described above, it is to be understood that the above embodiments are exemplary and are not to be construed as limitations of the present disclosure. A person skilled in the art may change, modify, replace and vary the above embodiments within the scope of the present disclosure.

Claims

1. A flight capability test platform, characterized in that: include: A flight simulation platform, wherein the flight simulation platform is used to simulate a flight state according to the flight data; A psychological quality evaluation device, which is arranged on the flight simulation platform and comprises: a first detection unit, which is used to detect physiological signals, and an output end of the first detection unit is connected to an input end of the flight simulation platform; A physical fitness assessment device, wherein the physical fitness assessment device is arranged on the flight simulation platform, and the physical fitness assessment device comprises: a pedal mechanism and a second detection unit, wherein the pedal mechanism is used to provide pedal feedback, and the second detection unit is used to detect the action signal of the pedal mechanism, and the output end of the second detection unit is connected to the input end of the flight simulation platform.

2. The flight capability test platform according to claim 1, characterized in that: The psychological quality assessment device also includes: A residual capacity test unit, the residual capacity test unit comprising: a plurality of test lights and a plurality of feedback buttons, the test lights and the feedback buttons are respectively arranged on the flight simulation platform, and the plurality of test lights and the plurality of feedback buttons correspond one to one; The input end of the test light is connected to the output end of the flight simulation platform, the output end of the feedback button is connected to the input end of the flight simulation platform, and the flight simulation platform is used to control at least one of the test lights to emit a test light, and record the delay time between the test light emitting the test light and the feedback button corresponding to the test light emitting a key signal.

3. The flight capability test platform according to claim 2, characterized in that: The psychological quality assessment device also includes: A stimulation unit, the stimulation unit comprising: an electrical stimulation vibration wristband, the electrical stimulation vibration wristband is used to electrically stimulate the wrist; Wherein, the input end of the electrical stimulation vibration wristband is connected to the output end of the flight simulation platform, and the flight simulation platform is used to control the electrical stimulation vibration wristband to perform electrical stimulation action when the delay time exceeds a preset time.

4. The flight capability test platform according to claim 1, characterized in that: The first detection unit comprises: A heart rate detection electrode, wherein the heart rate detection electrode is used to detect the heart rate, and an output end of the heart rate detection electrode is connected to an input end of the flight simulation platform, wherein the flight simulation platform is used to record the heart rate in real time and stop the flight simulation when the heart rate exceeds a preset heart rate range; and / or A skin resistance detection electrode, wherein the skin resistance detection electrode is used to detect skin resistance, and an output end of the skin resistance detection electrode is connected to an input end of the flight simulation platform, wherein the flight simulation platform is used to record the skin resistance in real time, and stop the flight simulation when the skin resistance exceeds a preset skin resistance range; and / or A body temperature detection probe, wherein the body temperature detection probe is used to detect body temperature, and an output end of the body temperature detection probe is connected to an input end of the flight simulation platform, wherein the flight simulation platform is used to record the body temperature in real time, and stop the flight simulation when the body temperature exceeds a preset body temperature range.

5. The flight capability test platform according to claim 1, characterized in that: The second detection unit comprises: A weighing sensor, wherein the weighing sensor is used to detect the pedaling force applied to the pedal mechanism, and the output end of the weighing sensor is connected to the input end of the flight simulation platform, wherein the flight simulation platform is used to record the pedaling force in real time, and simulate the flight state according to the pedaling force and the flight data; and / or a first angular displacement sensor, the first angular displacement sensor being used to detect the rudder deflection angle of the pedal mechanism under the pedal force, and the output end of the first angular displacement sensor being connected to the input end of the flight simulation platform, wherein the flight simulation platform is used to record the rudder deflection angle in real time, and simulate the flight state according to the rudder deflection angle and the flight data; and / or A second angular displacement sensor, wherein the second angular displacement sensor is used to detect the pedal deflection angle of the pedal mechanism under the action of pedal force, and the output end of the second angular displacement sensor is connected to the input end of the flight simulation platform, wherein the flight simulation platform is used to record the pedal deflection angle in real time, and simulate the flight state according to the pedal deflection angle and the flight data.

6. The flight capability test platform according to any one of claims 1 to 5, characterized in that: The flight simulation platform comprises: A cockpit, the cockpit comprising: a base, a front frame and a rear plate, the front frame and the rear plate are respectively arranged at two ends of the base, and the physical fitness evaluation device is arranged at one end of the base close to the front frame, and the psychological quality evaluation device is arranged at one end of the base close to the rear plate; A seat, the seat being arranged at one end of the base close to the rear plate; The simulation unit comprises: a host, a display and a control handle, the host and the display are respectively arranged on the front frame, and the display and the seat are arranged opposite to each other, the control handle is arranged on the seat, the input end of the host is respectively connected to the output end of the first detection unit, the output end of the second detection unit and the input end of the control handle, and the output end of the host is connected to the input end of the display.

7. The flight capability test platform according to claim 6, characterized in that: The flight simulation platform also includes: A shoulder pressing unit, wherein the shoulder pressing unit is arranged on the rear plate, and the shoulder pressing unit comprises: a lifting plate, at least one shoulder pressing plate and a driving assembly, wherein the lifting plate is slidingly arranged on the rear plate, the shoulder pressing plate is arranged on the lifting plate, the driving assembly is transmission-connected to the lifting plate, and the driving assembly is used to drive the lifting plate to lift and lower so that the shoulder pressing plate is against or away from the shoulder.

8. The flight capability test platform according to claim 7, characterized in that: The driving assembly comprises: a ball screw and at least one guide column, the ball screw is rotatably arranged on the rear plate, the guide column is arranged on the rear plate, the lifting plate is slidably arranged on the guide column, and the lifting plate and the ball screw are connected by threaded transmission; Wherein, the driving component further includes: A handwheel, the handwheel is connected to the ball screw in a transmission manner, and the handwheel is used to drive the ball screw to rotate so as to lift the lifting plate; and / or A motor control module, a motor drive module and a shoulder press motor, wherein the input end of the motor control module is connected to the output end of the host, and the output end of the motor control module is connected to the input end of the motor drive module, the output end of the motor drive module is connected to the input end of the shoulder press motor, the shoulder press motor is transmission-connected to the ball screw, and the shoulder press motor is used to drive the ball screw to rotate so as to lift the lifting plate.

9. The flight capability test platform according to claim 7, characterized in that: The shoulder pressing plate is rotatably arranged on the lifting plate, and a damper is arranged between the shoulder pressing plate and the lifting plate.

10. The flight capability test platform according to claim 6, characterized in that: The simulation unit also includes: An indicator light, the indicator light is arranged on the front frame and / or the rear panel, and an input end of the indicator light is connected to an output end of the host; and / or A speaker, wherein the speaker is arranged on the front frame and / or the rear panel, and an input end of the speaker is connected to an output end of the host; and / or A mouse, wherein the mouse is arranged on the front frame, and an output end of the mouse is connected to an input end of the host; and / or A keyboard is arranged on the front frame, and an output end of the keyboard is connected to an input end of the host.

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