CN217306012U - Aircraft course attitude instrument simulation training device - Google Patents
Aircraft course attitude instrument simulation training device Download PDFInfo
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- CN217306012U CN217306012U CN202122274820.8U CN202122274820U CN217306012U CN 217306012 U CN217306012 U CN 217306012U CN 202122274820 U CN202122274820 U CN 202122274820U CN 217306012 U CN217306012 U CN 217306012U
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Abstract
The application discloses real device of instructing of aircraft course gesture instrument simulation compares with prior art, includes: an operation panel for setting flight parameters; the aircraft course attitude simulation device is connected with the operation panel; the aircraft course attitude simulation device simulates the flight state of the aircraft according to the flight parameters; the interface circuit is arranged between the operation panel and the aircraft course attitude simulation device; the data control device is connected with the aircraft course attitude simulation device; the real course attitude instrument assembly is connected with the data control device and is used for displaying the real course attitude of the airplane and the real course attitude parameters in real time; and the virtual course attitude instrument component is connected with the real course attitude instrument component in parallel and synchronously displays the course and the attitude parameters of the airplane in real time. Compared with the prior art, the method can simulate the airplane state of the airplane, realize accurate control of the course attitude of the airplane, and avoid the problems of high cost and high risk of real airplane test run.
Description
Technical Field
The application relates to the technical field of simulated practical training devices, in particular to a simulated practical training device for an aircraft heading attitude instrument.
Background
The simulation training of the airplane is an essential course for a flight beginner. For flight beginners, after theoretical knowledge learning is finished, great potential safety hazards exist if entity training is directly carried out, and once accidents occur, economic losses caused by the accidents are immeasurable. In this case, a device for simulating practical training of an airplane is developed. .
At present, aiming at the course attitude simulation training of an airplane, if a real airplane is adopted for demonstration, the operation is very complicated, the cost is very expensive, and the safety and the reliability can not be effectively guaranteed; if the training device is adopted for training, the training device generally needs to be provided with a simulation cabin, a motion system and a vision system, and each component of the training device is expensive in acquisition cost, complex in operation, not beneficial to direct hands-on training of a novice and low in practicability; some virtual simulation is directly performed in a VR mode, but the practical training effect is not visual, and operability and feasibility are lacked.
Therefore, how to provide an aircraft heading attitude instrument simulation practical training device, which can simulate the aircraft state of an aircraft, realize accurate control of the aircraft heading attitude, and avoid the problems of high cost and high risk of real aircraft commissioning, has become a technical problem to be solved urgently by technical staff in the field.
SUMMERY OF THE UTILITY MODEL
In order to solve the technical problems, the application provides an aircraft course attitude instrument simulation practical training device which can simulate the aircraft state of an aircraft, realize accurate control on the aircraft course attitude and avoid the problems of high cost and high risk of real aircraft test run.
The technical scheme provided by the application is as follows:
the application provides real device of instructing of aircraft course gesture instrument simulation includes: an operation panel for setting flight parameters; the aircraft course attitude simulation device is connected with the operation panel; the aircraft course attitude simulation device simulates the flight state of the aircraft according to the flight parameters; the interface circuit is arranged between the operation panel and the aircraft course attitude simulation device; the interface circuit is used for transmitting a control signal to the aircraft course attitude simulation device to realize signal interaction; the data control device is connected with the aircraft course attitude simulation device; the real course attitude instrument assembly is connected with the data control device and is used for displaying the real course attitude of the airplane and the real course attitude parameters in real time; and the virtual course attitude instrument component is connected with the real course attitude instrument component in parallel and synchronously displays the course and the attitude parameters of the airplane in real time.
Further, in a preferred mode of the present invention, the operation panel includes:
an operation interface; a course attitude management platform is arranged on the operation interface and used for adjusting the control mode of the practical training device; a flight parameter presetting system connected with the operation interface and used for configuring flight parameters;
and the flight parameter presetting system presets and transmits corresponding control signals to the aircraft course attitude simulation device according to the current parameters.
Further, in a preferred mode of the present invention, the aircraft heading attitude simulation apparatus includes:
the rotary table control assembly is connected with the interface circuit and used for generating an operation instruction according to the control signal;
the three-axis rotary table is connected with the rotary table control assembly and is used for simulating the course and the posture of the airplane based on the operating instruction;
the gyroscope assembly is connected with the three-axis turntable and used for sensing the real motion vector parameters of the three-axis turntable and converting the real motion vector parameters into corresponding electric signals;
and a frame for supporting the turret control assembly, the three-axis turret, and the gyro assembly.
Further, in a preferred mode of the present invention, the aircraft heading attitude simulation apparatus further includes:
the roll rotating assembly is used for adjusting roll according to the zeroing and angle operating instruction output by the turntable control assembly;
the pitching rotating assembly carries out pitching adjustment according to the zeroing and angle operating instruction output by the turntable control assembly;
the course rotating assembly is used for carrying out course adjustment according to the zeroing and angle operation instruction output by the turntable control assembly;
the roll rotating assembly, the pitching rotating assembly and the course rotating assembly are all connected with the turntable control assembly.
Further, in a preferred mode of the present invention, the gyro assembly is specifically a three-degree-of-freedom gyro; the gyro component is used for sensing the real motion vector parameters of the roll rotating system, the pitch rotating system and the course rotating system and outputting corresponding electric signals.
Further, in a preferred mode of the present invention, the data management and control device includes:
the data analysis unit is connected with the aircraft course attitude simulation device;
the data analysis unit is connected with the gyro assembly, carries out algorithm analysis according to the course and attitude vector signals output by the gyro assembly, and demodulates the real flight parameters of the three-axis turntable;
the data comparison unit is connected with the data analysis unit; and the real heading attitude instrument indication calculation unit and the virtual heading attitude instrument indication calculation unit are connected with the data comparison unit.
Further, in a preferred mode of the present invention, the real heading attitude instrument indicating and calculating unit is connected to the real heading attitude instrument assembly; the virtual course attitude instrument indication calculation unit is connected with the virtual course attitude instrument assembly.
Further, in a preferred mode of the present invention, the real heading attitude component includes:
the follow-up system is connected with the data control device and used for carrying out remote transmission;
the azimuth instrument and the attitude instrument are connected with the servo system and used for indicating the real course and the real attitude of the airplane in real time; and the instrument external expansion circuit and the fault management unit are connected with the follow-up system.
Further, in a preferred mode of the present invention, the virtual heading instrument assembly includes: a main flight display PFD and a navigation display ND which are connected with the data control device; the main flight display PFD and the navigation display ND display flight parameters completely synchronized with the azimuth and the attitude indicator in real time.
The utility model provides a pair of real device of instructing of aircraft course gesture instrument simulation compares with prior art, include: an operation panel for setting flight parameters; the aircraft course attitude simulation device is connected with the operation panel; the aircraft course attitude simulation device simulates the flight state of the aircraft according to the flight parameters; the interface circuit is arranged between the operation panel and the aircraft course attitude simulation device; the interface circuit is used for transmitting a control signal to the aircraft course attitude simulation device to realize signal interaction; the data control device is connected with the aircraft course attitude simulation device; the real course attitude instrument component is connected with the data control device and is used for displaying the course and the attitude parameters of the airplane in real time; and the virtual course attitude instrument component is connected with the real course attitude instrument component in parallel and synchronously displays the course and the attitude parameters of the airplane in real time. In the simulation training process, the flight parameters such as course, attitude and the like are set by using the operation panel; the aircraft course attitude simulation device demonstrates various flight states of the aircraft in real time according to the flight parameters; then, analyzing and calculating the real flight parameters of the aircraft course attitude simulation device through the data control device, and comparing and correcting the real flight parameters with preset theoretical flight parameters; the corrected data is synchronously displayed by the real course attitude instrument component and the virtual course attitude instrument component in real time, and the whole process of simulating practical training is completed. The utility model relates to a technical scheme compares in prior art, and its aircraft state that can simulate the aircraft realizes the accurate control to aircraft course gesture, avoids the costly and high risk problem of real aircraft taking a trial run.
The utility model has the advantages that:
the utility model provides an aircraft course attitude instrument simulation training device, which utilizes the operation panel to set flight parameters such as course, attitude and the like on an operation interface; the aircraft course attitude simulation device demonstrates various flight states of the aircraft in real time according to the flight parameters; then, analyzing and calculating the real flight parameters of the aircraft course attitude simulation device through the data control device, and comparing and correcting the real flight parameters with preset theoretical flight parameters; the corrected data is synchronously displayed by the real course attitude instrument component and the virtual course attitude instrument component in real time, so that the practicability, the verisimilitude, the safety, the reliability, the visibility and the feasibility of the practical training device are improved, and the problems of high cost, high risk and the like of real aircraft test run are solved.
Drawings
In order to more clearly illustrate the embodiments of the present application or the technical solutions in the prior art, the drawings used in the description of the embodiments or the prior art will be briefly described below, it is obvious that the drawings in the following description are only some embodiments of the present application, and for those skilled in the art, other drawings can be obtained according to the drawings without creative efforts.
Fig. 1 is a block diagram of the practical training device for simulating the aircraft heading attitude instrument in the embodiment of the utility model;
fig. 2 is a block diagram of the schematic structure of the device for simulating the course attitude of an aircraft according to an embodiment of the present invention;
fig. 3 is a block diagram schematically illustrating a structure of a data management and control apparatus according to an embodiment of the present invention;
fig. 4 is a block diagram of the structure of the real heading attitude instrument assembly in the embodiment of the present invention.
Description of reference numerals:
an operation panel 1; an operation interface 101; a flight parameter presetting system 102; an interface circuit 2; an aircraft course attitude simulation device 3; a data management and control device 4; a real course attitude instrument assembly 5; a virtual course attitude instrument assembly 6; a primary flight display PFD 601; a navigation display ND 602; a turntable control assembly 7; a three-axis turntable 8; a gyro assembly 9; a roll rotation assembly 10; a pitch rotating assembly 11; a course rotating assembly 12; a data analysis unit 13; a data comparing unit 14; a real course attitude instrument indication calculation unit 15; a virtual heading attitude instrument indication calculation unit 16; a servo system 17; an azimuth meter 18; an attitude instrument 19; a fault management unit 20; an instrument extension circuit 21.
Detailed Description
In order to make those skilled in the art better understand the technical solutions in the present application, the technical solutions in the embodiments of the present application will be clearly and completely described below with reference to the drawings in the embodiments of the present application, and it is obvious that the described embodiments are only a part of the embodiments of the present application, and not all embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present application.
It will be understood that when an element is referred to as being "fixed" or "disposed" on another element, it can be directly on the other element or be indirectly disposed on the other element; when an element is referred to as being "connected to" another element, it can be directly connected to the other element or be indirectly connected to the other element.
It will be understood that the terms "length," "width," "upper," "lower," "front," "rear," "first," "second," "vertical," "horizontal," "top," "bottom," "inner," "outer," and the like, are used herein to indicate an orientation or positional relationship, which is based on the orientation or positional relationship shown in the drawings, but merely to facilitate the description and simplify the description, and are not intended to indicate or imply that the device or element so referred to must have a particular orientation, be constructed and operated in a particular orientation, and are not to be construed as limiting the application.
Furthermore, the terms "first", "second" and "first" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance or implicitly indicating the number of technical features indicated. Thus, a feature defined as "first" or "second" may explicitly or implicitly include one or more of that feature. In the description of the present application, "plurality" or "a plurality" means two or more unless specifically limited otherwise.
It should be understood that the structures, ratios, sizes, and the like shown in the drawings are only used for matching the disclosure of the specification, so as to be understood and read by those skilled in the art, and are not used to limit the practical limit conditions of the present application, so that the modifications of the structures, the changes of the ratio relationships, or the adjustment of the sizes, do not have the technical essence, and the modifications, the changes of the ratio relationships, or the adjustment of the sizes, are all within the scope of the technical contents disclosed in the present application without affecting the efficacy and the achievable purpose of the present application.
Please show as fig. 1 to 4, the embodiment of the present invention provides an aircraft course attitude instrument simulation training device, including: an operation panel 1 for setting flight parameters; the aircraft course attitude simulation device 3 is connected with the operation panel 1; the aircraft course attitude simulation device 3 simulates the flight state of the aircraft according to the flight parameters; the interface circuit 2 is arranged between the operation panel 1 and the aircraft course attitude simulation device 3; the interface circuit 2 is used for transmitting a control signal to the aircraft course attitude simulation device 3 to realize signal interaction; the data management and control device 4 is connected with the aircraft course attitude simulation device 3; the real course attitude instrument component 5 is connected with the data control device 4 and is used for displaying the course and the attitude parameters of the airplane in real time; and the virtual course attitude instrument component 6 is arranged in parallel with the real course attitude instrument component 5 and synchronously displays the course and the attitude parameters of the airplane in real time.
The embodiment of the utility model provides a provide a pair of real device of instructing of aircraft course gesture instrument simulation that the embodiment provides, include: an operation panel 1 for setting flight parameters; the aircraft course attitude simulation device 3 is connected with the operation panel 1; the aircraft course attitude simulation device 3 simulates the flight state of the aircraft according to the flight parameters; the interface circuit 2 is arranged between the operation panel 1 and the aircraft course attitude simulation device 3; the interface circuit 2 is used for transmitting a control signal to the aircraft course attitude simulation device 3 to realize signal interaction; the data management and control device 4 is connected with the aircraft course attitude simulation device 3; the real course attitude instrument component 5 is connected with the data control device 4 and is used for displaying the course and the attitude parameters of the airplane in real time; and the virtual course attitude instrument component 6 is arranged in parallel with the real course attitude instrument component 5 and synchronously displays the course and the attitude parameters of the airplane in real time. In the simulation training process, the flight parameters such as course, attitude and the like are set by using the operation panel 1; the aircraft course attitude simulation device 3 demonstrates various flight states of the aircraft in real time according to the flight parameters; then, analyzing and calculating the real flight parameters of the aircraft heading and attitude simulation device 3 through the data management and control device 4, and comparing the real flight parameters with preset theoretical flight parameters and correcting and calibrating the real flight parameters; the corrected data is synchronously displayed by the real course attitude instrument component 5 and the virtual course attitude instrument component 6 in real time, and the whole process of simulating practical training is completed. The utility model relates to a technical scheme compares in prior art, and its aircraft state that can simulate the aircraft realizes the accurate control to aircraft course gesture, avoids the costly and high risk problem of real aircraft taking a trial run.
Specifically, in the embodiment of the present invention, the operation panel 1 includes:
an operation interface 101; a course attitude management platform is arranged on the operation interface 101 and used for adjusting a control mode of the practical training device; a flight parameter presetting system 102 connected with the operation interface 101 and configured with flight parameters;
the flight parameter presetting system 102 transmits a corresponding control signal to the aircraft course attitude simulation device 3 according to the current parameter presetting.
The course attitude management platform is arranged on the operation interface 101, and two modes of manual control and automatic control can be selected; the flight parameter presetting system 102 manually sets or automatically calls out theoretical flight parameters according to the motion mode selected by the operation interface 101, and then outputs corresponding control signals to the aircraft heading and attitude simulation device 3 through the interface circuit 2.
Specifically, in the embodiment of the present invention, the aircraft heading attitude simulation apparatus 3 includes:
the rotary table control component 7 is connected with the interface circuit 2 and used for generating an operation instruction according to the control signal;
the three-axis turntable 8 is connected with the turntable control assembly 7, and the three-axis turntable 8 simulates the course and the posture of the airplane based on the operation instruction;
the gyroscope assembly 9 is connected with the three-axis turntable 8, and the gyroscope assembly 9 is used for sensing the real motion vector parameters of the three-axis turntable 8 and converting the real motion vector parameters into corresponding electric signals;
and a frame for supporting said turret control assembly 7, said three-axis turret 8 and said gyroscopic assembly 9.
Specifically, in the embodiment of the present invention, the aircraft heading attitude simulation apparatus 3 further includes:
the roll rotating assembly 10 is used for adjusting roll according to the zeroing and angle operating instruction output by the rotary table control assembly 7 through the roll rotating assembly 10;
the pitching rotating component 11 performs pitching adjustment according to the zeroing and angle operating instruction output by the turntable control component 7;
the course rotating component 12 is used for carrying out course adjustment according to the zeroing and angle operation instruction output by the rotary table control component 7 by the course rotating component 12;
the roll rotating component 10, the pitch rotating component 11 and the course rotating component 12 are all connected with the turntable control component 7.
The aircraft course attitude simulation device 3 is composed of a plurality of functional components according to different functions required to be realized; the turntable control component 7 mainly receives a control signal transmitted by the flight parameter presetting system 102, and generates a corresponding operation instruction based on the control signal;
then, according to the type of the operation instruction, the roll rotating assembly 10, the pitch rotating assembly 11 or the course rotating assembly 12 drives the three-axis turntable 8 to complete the adjustment of the corresponding flight course or attitude;
and finally, the gyro assembly 9 outputs an electric signal to the data management and control device 4 according to the real motion vector parameter of the roll rotating system, the pitch rotating system or the course rotating system.
Specifically, in the embodiment of the present invention, the gyro assembly 9 is specifically a three-degree-of-freedom gyro; the gyro assembly 9 is used for sensing the real motion vector parameters of the roll rotating system, the pitch rotating system and the course rotating system and outputting corresponding electric signals.
The aircraft course attitude simulation device 3 is used for transmitting control signals output by a manual or automatic theoretical flight mode and parameters arranged on the operation panel 1 to the turntable control component 7, so that operation instructions are generated to control the three-axis turntable 8 in roll, pitch, zero returning of course, angle, amplitude and the like, and then the three-degree-of-freedom gyroscope component 9 is used for sensing real motion vector parameters of the three-axis turntable 8 and outputting corresponding electric signals, so that simulation training of the aircraft course attitude is completed.
Specifically, in the embodiment of the present invention, the data management and control device 4 includes:
the data analysis unit 13 is connected with the aircraft course attitude simulation device 3;
the data analysis unit 13 is connected with the gyro assembly 9, and performs algorithm analysis according to the course and attitude vector signals output by the gyro assembly 9 to demodulate the real flight parameters of the three-axis turntable 8;
a data comparing unit 14 connected to the data analyzing unit 13; a real heading attitude instrument indication calculating unit 15 and a virtual heading attitude instrument indication calculating unit 16 which are connected with the data comparison unit 14.
The data management and control device 4 is configured to perform data analysis on the real motion vector signal of the three-axis turntable 8 output by the aircraft heading and attitude simulation device 3, and demodulate the real flight parameters of the three-axis turntable 8; and the data comparison unit 14 is used for comparing the data with a preset theoretical value, and the data are respectively output to the real course attitude instrument component 5 and the virtual course attitude instrument component 6 after calculation and error correction so as to ensure the accuracy, identity and stability of the data of the real course attitude instrument component and the virtual course attitude instrument component.
Specifically, in the embodiment of the present invention, the real heading attitude instrument indication calculation unit 15 is connected to the real heading attitude instrument assembly 5; the virtual heading attitude instrument indication calculation unit 16 is connected with the virtual heading attitude instrument assembly 6.
Specifically, in the embodiment of the utility model, real course gesture subassembly includes:
a follow-up system 17 connected with the data management and control device 4 for remote transmission;
an azimuth instrument 18 and an attitude instrument 19 which are connected with the servo system 17 and used for indicating the real course and attitude of the airplane in real time; and a meter extension circuit 21 and a fault management unit 20 connected to the slave system 17.
The real course attitude instrument component 5 is used for analyzing, calculating and correcting the real flight parameters of the aircraft course attitude simulation training device by the data management and control device 4, and then remotely transmitting the analyzed, calculated and corrected real flight parameters by the follow-up system 17 to drive the azimuth instrument 18 and the attitude instrument 19 to indicate the real course and attitude of the aircraft in real time, and meanwhile, the instrument external expansion circuit 21 and the fault management unit 20 can provide standard electric signals for the external hanging type real aircraft course and attitude instrument 19, so that the detection, inspection and maintenance of the real instrument are facilitated, the circuit fault can be set, and the circuit of the course attitude instrument 19 can be developed for the second time.
Specifically, in the embodiment of the present invention, the virtual heading instrument assembly includes: a primary flight display PFD601 and a navigation display ND602 connected to the data management and control device 4; the primary flight display PFD601 and the navigation display ND602 display in real time the flight parameters perfectly synchronized with the azimuth 18 and the attitude indicator 19.
To sum up, the utility model provides a simulation training device for aircraft course attitude instruments, which utilizes the operation panel 1 to set flight parameters such as course, attitude and the like on the operation interface 101 in the simulation training process; the aircraft course attitude simulation device 3 demonstrates various flight states of the aircraft in real time according to flight parameters; then, the real flight parameters of the aircraft heading and attitude simulation device 3 are analyzed and calculated through the data control device 4, and are compared with preset theoretical flight parameters and corrected and calibrated; the corrected data is synchronously displayed by the real course attitude instrument component 5 and the virtual course attitude instrument component 6 in real time, so that the practicability, verisimilitude, safety, reliability, visibility and feasibility of the practical training device are improved, and the problems of high cost, high risk and the like of real airplane test run are solved.
The previous description of the disclosed embodiments is provided to enable any person skilled in the art to make or use the present invention. Various modifications to these embodiments will be readily apparent to those skilled in the art, and the generic principles defined herein may be applied to other embodiments without departing from the spirit or scope of the invention. Thus, the present invention is not intended to be limited to the embodiments shown herein but is to be accorded the widest scope consistent with the principles and novel features disclosed herein.
Claims (9)
1. The utility model provides an aircraft course gesture instrument simulation real training device which characterized in that includes:
an operation panel for setting flight parameters;
the aircraft course attitude simulation device is connected with the operation panel;
the aircraft course attitude simulation device simulates the flight state of the aircraft according to the flight parameters;
the interface circuit is arranged between the operation panel and the aircraft course attitude simulation device; the interface circuit is used for transmitting a control signal to the aircraft course attitude simulation device to realize signal interaction;
the data control device is connected with the aircraft course attitude simulation device;
the real course attitude instrument component is connected with the data control device and is used for displaying the course and the attitude parameters of the airplane in real time; and the virtual course attitude instrument component is connected with the real course attitude instrument component in parallel and synchronously displays the course and the attitude parameters of the airplane in real time.
2. The aircraft heading attitude instrument simulation training device according to claim 1, wherein the operation panel comprises:
an operation interface; a course attitude management platform is arranged on the operation interface and used for adjusting the control mode of the practical training device; a flight parameter presetting system connected with the operation interface and used for configuring flight parameters;
and the flight parameter presetting system is used for presetting and transmitting corresponding control signals to the aircraft course attitude simulation device according to the current parameters.
3. The aircraft heading attitude instrument simulation training device according to claim 1, wherein the aircraft heading attitude simulation device comprises:
the rotary table control assembly is connected with the interface circuit and used for generating an operation instruction according to the control signal;
the three-axis rotary table is connected with the rotary table control assembly and is used for simulating the course and the posture of the airplane based on the operation instruction;
the gyroscope assembly is connected with the three-axis turntable and used for sensing the real motion vector parameters of the three-axis turntable and converting the real motion vector parameters into corresponding electric signals;
and a frame for supporting the turret control assembly, the three-axis turret, and the gyro assembly.
4. The aircraft heading attitude instrument simulation training device according to claim 3, further comprising:
the roll rotating assembly is used for adjusting roll according to the zeroing and angle operating instruction output by the turntable control assembly;
the pitching rotating assembly carries out pitching adjustment according to the zeroing and angle operating instruction output by the turntable control assembly;
the course rotating assembly is used for carrying out course adjustment according to the zeroing and angle operation instruction output by the rotary table control assembly;
the roll rotating assembly, the pitching rotating assembly and the course rotating assembly are all connected with the turntable control assembly.
5. The aircraft heading attitude instrument simulation practical training device according to claim 4, wherein the gyro component is specifically a three-degree-of-freedom gyro; the gyro component is used for sensing the real motion vector parameters of the roll rotating system, the pitch rotating system and the course rotating system and outputting corresponding electric signals.
6. The aircraft heading attitude instrument simulation training device according to claim 3, wherein the data management and control device comprises:
the data analysis unit is connected with the aircraft course attitude simulation device;
the data analysis unit is connected with the gyro assembly, carries out algorithm analysis according to the course and attitude vector signals output by the gyro assembly, and demodulates the real flight parameters of the three-axis turntable;
the data comparison unit is connected with the data analysis unit; and the real heading attitude instrument indication calculation unit and the virtual heading attitude instrument indication calculation unit are connected with the data comparison unit.
7. The aircraft heading attitude instrument simulation training device according to claim 6, wherein the real heading attitude instrument indication calculation unit is connected with the real heading attitude instrument component; the virtual course attitude instrument indication calculation unit is connected with the virtual course attitude instrument assembly.
8. The aircraft heading attitude instrument simulation training device according to claim 1, wherein the real heading attitude instrument assembly comprises:
the follow-up system is connected with the data control device and used for carrying out remote transmission;
the azimuth instrument and the attitude instrument are connected with the servo system and used for indicating the real course and the real attitude of the airplane in real time; and the meter external expansion circuit and the fault management unit are connected with the follow-up system.
9. The aircraft heading attitude instrument simulation training device according to claim 8, wherein the virtual heading attitude instrument assembly comprises: the main flight display PFD and the navigation display ND are connected with the data management and control device; the main flight display PFD and the navigation display ND display flight parameters completely synchronized with the azimuth and the attitude indicator in real time.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202122274820.8U CN217306012U (en) | 2021-10-21 | 2021-10-21 | Aircraft course attitude instrument simulation training device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202122274820.8U CN217306012U (en) | 2021-10-21 | 2021-10-21 | Aircraft course attitude instrument simulation training device |
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| Publication Number | Publication Date |
|---|---|
| CN217306012U true CN217306012U (en) | 2022-08-26 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN202122274820.8U Active CN217306012U (en) | 2021-10-21 | 2021-10-21 | Aircraft course attitude instrument simulation training device |
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| CN (1) | CN217306012U (en) |
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- 2021-10-21 CN CN202122274820.8U patent/CN217306012U/en active Active
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