CN110992767A - Simulated aircraft control system - Google Patents
Simulated aircraft control system Download PDFInfo
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- CN110992767A CN110992767A CN202010010526.3A CN202010010526A CN110992767A CN 110992767 A CN110992767 A CN 110992767A CN 202010010526 A CN202010010526 A CN 202010010526A CN 110992767 A CN110992767 A CN 110992767A
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- G09—EDUCATION; CRYPTOGRAPHY; DISPLAY; ADVERTISING; SEALS
- G09B—EDUCATIONAL OR DEMONSTRATION APPLIANCES; APPLIANCES FOR TEACHING, OR COMMUNICATING WITH, THE BLIND, DEAF OR MUTE; MODELS; PLANETARIA; GLOBES; MAPS; DIAGRAMS
- G09B9/00—Simulators for teaching or training purposes
- G09B9/02—Simulators for teaching or training purposes for teaching control of vehicles or other craft
- G09B9/08—Simulators for teaching or training purposes for teaching control of vehicles or other craft for teaching control of aircraft, e.g. Link trainer
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Abstract
The invention discloses a simulated aircraft control system, which comprises: the system comprises a flight control system, a motion simulation subsystem, a visual simulation subsystem, a sound simulation subsystem, a manipulation simulation subsystem, a boarding simulation subsystem and an instructor console; the flight control system is used for receiving and analyzing signals from the manipulation simulation subsystem and signals from the instructor console to obtain control instructions of each simulation subsystem and outputting the control instructions to each simulation subsystem; each simulation subsystem receives respective control instruction to execute corresponding instruction; the teacher control console is used for power control, aircraft state monitoring and setting simulation, environment control, fault setting and training course setting during training. The simulated aircraft control system provided by the invention realizes the coordination control of each subsystem.
Description
Technical Field
The invention relates to the technical field of simulated aircrafts, in particular to a simulated aircraft control system.
Background
With the application and development of modern scientific technology in the military field, the destructive power of weaponry is continuously increased, so that the practical use of actual equipment, actual soldiers and actual bullets in military training activities is increasingly limited, and simultaneously, advanced and practical technical conditions are provided for military training by adopting an analog means. For flight training, the content is large, the difficulty is high, and the risk is high. Therefore, the flight training means is more necessary and urgent to realize simulation.
Currently, a flight simulator is a modern training device for realizing the simulation of a training means. The strength and experience of the air force and the navy are in the leading position in China in the aspects of development, use, teaching, maintenance, development of simulated flight training and the like of flight simulators.
In the development process of the flight simulator, how to design the control system of the flight simulator, and further perform coordinated fusion control on each subsystem, and finally provide the pilot with the need to perform various simulations is a problem that needs to be solved by those skilled in the art urgently.
Disclosure of Invention
In view of this, the invention provides a simulated aircraft control system, which realizes the coordination control of each subsystem.
In order to achieve the purpose, the invention adopts the following technical scheme:
a simulated aircraft control system comprising: the system comprises a flight control system, a motion simulation subsystem, a visual simulation subsystem, a sound simulation subsystem, a manipulation simulation subsystem, a boarding simulation subsystem and an instructor console;
the flight control system is used for receiving and analyzing signals from the manipulation simulation subsystem and signals from the instructor console to obtain control instructions of each simulation subsystem and outputting the control instructions to each simulation subsystem;
each simulation subsystem receives respective control instruction to execute corresponding instruction;
the teacher control console is used for power control, aircraft state monitoring and setting simulation, environment control, fault setting and training course setting during training.
Preferably, the method further comprises the following steps: an evaluation system coupled to the instructor console;
the evaluation system is used for receiving flight data of the simulated aircraft, storing the flight data into the database, and comparing and operating the flight data with parameters stored in the standard database in advance to obtain an evaluation result; and storing the evaluation result in the database, and sending the evaluation result to the instructor console for reference and calling by an instructor.
Preferably, the method further comprises the following steps: the downloading module is connected with the instructor console;
the downloading module is used for downloading flight data of the simulation training according to the input personnel information.
Preferably, the manipulation simulation subsystem includes: the aerobridge comprises a aerobridge operating lever, a rudder, a force servo actuating mechanism and an auxiliary operating system;
the boarding bridge operating rod is used for operating a boarding bridge;
the rudder is connected to the force servo actuator through a transmission mechanism, and a sensor is mounted on the transmission mechanism; the sensor is used for acquiring force applied to the rudder and displacement and rotation angle generated by the force;
the boarding bridge operating lever, the rudder, the force servo actuating mechanism and the auxiliary operating system are all connected with the flight control system.
Preferably, the boarding simulation subsystem includes: the boarding control system comprises a boarding controller, an alarm lamp, an upper sensor and a lower sensor; the boarding controller is connected with the flight control system;
the alarm lamp, the upper sensor and the lower sensor are all connected with the boarding controller;
the boarding controller is used for controlling the boarding bridge to take off and land based on the boarding bridge joystick;
the alarm lamp is used for indicating the state of the boarding bridge;
the upper sensor is used for detecting the highest position of the boarding bridge;
the lower sensor is used for detecting the lowest position of the boarding bridge.
Preferably, the auxiliary control system comprises a front wheel turning simulation control device and a brake simulation control device which are connected with the flight control system through sensors.
Preferably, the sensor is connected to the flight control system by a signal processing circuit.
Preferably, the signal processing circuit includes: the device comprises a filter circuit, an amplifying circuit, an analog-to-digital conversion circuit and a level conditioning circuit;
the force information, the displacement information and the rotation angle information collected by the sensor are transmitted to the flight control system through the filter circuit, the amplifying circuit, the analog-to-digital conversion circuit and the level conditioning circuit in sequence.
According to the technical scheme, compared with the prior art, the invention discloses and provides a simulated aircraft control system which mainly comprises a flight control system, a motion simulation subsystem, a visual simulation subsystem, a sound simulation subsystem, a manipulation simulation subsystem, a boarding simulation subsystem and a teacher console; the flight control system analyzes the signals, controls each simulation subsystem according to the analyzed signals, further implements corresponding actions, and realizes the coordination control of each subsystem.
Drawings
FIG. 1 is a first schematic diagram of a simulated aircraft control system provided by the present invention;
FIG. 2 is a second schematic diagram of a simulated aircraft control system provided by the present invention;
FIG. 3 is a third schematic diagram of a simulated aircraft control system provided by the present invention;
FIG. 4 is a schematic diagram of the components of a steering simulation subsystem provided by the present invention;
fig. 5 is a schematic diagram of the composition of a boarding simulation subsystem provided by the present invention;
FIG. 6 is a block diagram of a signal processing circuit according to the present invention;
fig. 7 is a circuit diagram of a signal processing circuit according to an embodiment of the present invention.
Detailed Description
The technical solution in the embodiments of the present invention will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present invention.
Referring to fig. 1, an embodiment of the present invention discloses a simulated aircraft control system, including: the system comprises a flight control system 1, a motion simulation subsystem 2, a visual simulation subsystem 3, a sound simulation subsystem 4, a control simulation subsystem 5, a boarding simulation subsystem 6 and an instructor console 7;
the flight control system 1 is used for receiving and analyzing signals from the manipulation simulation subsystem 5 and signals from the instructor console 7 to obtain control instructions of each simulation subsystem and outputting the control instructions to each simulation subsystem;
each simulation subsystem receives respective control instruction to execute corresponding instruction;
the instructor console 7 is used for power control, aircraft state monitoring and setting simulation, environmental control, fault setting and training course setting when training is completed.
The invention discloses and provides a simulated aircraft control system, which mainly comprises a flight control system 1, a motion simulation subsystem 2, a visual simulation subsystem 3, a sound simulation subsystem 4, a control simulation subsystem 5, a boarding simulation subsystem 6 and a teacher console 7; the flight control system 1 analyzes the signals, and controls each analog subsystem according to the analyzed signals, so as to implement corresponding actions, thereby realizing the coordination control of each subsystem.
Referring to fig. 2, in order to further optimize the above technical solution, the method further includes, on the basis of the above embodiment: an evaluation system 8, said evaluation system 8 being connected to said instructor console 7;
the evaluation system 8 is used for receiving flight data of the simulated aircraft, storing the flight data into a database, and comparing and operating the flight data with parameters stored in a standard database in advance to obtain an evaluation result; and storing the evaluation result in the database, and sending the evaluation result to the instructor console 7 for reference and calling by an instructor.
The simulated aircraft control system provided by the invention can evaluate according to the data acquired in the simulated training process of a trainer, objectively evaluate the training quality of the flight of the simulated aircraft, avoid the condition that the evaluation is not uniform due to the large difference of the evaluation caused by overlarge subjective evaluation of manual evaluation, and meanwhile, further know the defects of the trainer in the training process from the data perspective by storing and analyzing the data, thereby improving the teaching quality.
Referring to fig. 3, in order to further optimize the above technical solution, the method further includes, on the basis of the above embodiment: the downloading module 9, the downloading module 9 is connected with the instructor console 7;
the downloading module 9 is used for downloading flight data of simulation training according to the input personnel information.
When wanting to see the training data of a certain training person, can input training person's information to derive all training data about this training person through download module 9, so that carry out subsequent analysis, with the achievement and the problem that exists of understanding simulation flight training more comprehensively, convenient pertinence is explained and is corrected, improves the teaching quality.
Referring to fig. 4, in order to further optimize the above technical solution, the manipulation simulation subsystem 5 is further defined on the basis of the above embodiment and includes: a boarding bridge operating lever 51, a rudder 52, a force servo actuator 53 and an auxiliary operating system 54;
the boarding bridge operating rod 51 is used for operating a boarding bridge;
the rudder 52 is connected to the force servo actuator 53 through a transmission mechanism, and a sensor is mounted on the transmission mechanism; wherein the sensor is used for collecting the force applied on the rudder 52 and the generated displacement and rotation angle;
the boarding bridge joystick 51, the rudder 52, the force servo actuator 53 and the auxiliary steering system 54 are all connected to the flight control system 1.
The sensors mounted on the control mechanism are used for measuring signals such as force, displacement and rotation angle, control instructions added on the force servo actuator 53 are obtained based on the signals, and corresponding force is generated based on the control instructions and loaded on the control mechanism, so that a trainer obtains real experience of flying vehicle driving.
Referring to fig. 5, in order to further optimize the above technical solution, the boarding simulation subsystem 6 is further defined to include, on the basis of the above embodiment: an boarding controller 61, a warning lamp 62, an upper sensor 63, and a lower sensor 64; the boarding controller 61 is connected with the flight control system 1;
the alarm lamp 62, the upper sensor 63 and the lower sensor 64 are all connected with the boarding controller 61;
the boarding controller 61 is used for controlling the boarding bridge to take off and land based on the boarding bridge operating rod 51;
the alarm lamp 62 is used for indicating the state of the boarding bridge;
the upper sensor 63 is used for detecting the highest position of the boarding bridge;
the lower sensor 64 is used to detect the lowest position of the boarding bridge.
The boarding bridge is controlled through the boarding simulation subsystem 6, the operation is more convenient, and the highest position and the lowest position of the lifting of the boarding bridge can be detected, so that the boarding bridge is safer. The automatically controlled mode of the boarding bridge facilitates the use of the simulated aircraft.
Referring to fig. 4, in order to further optimize the above technical solution, it is further defined on the basis of the above embodiment that the auxiliary operating system 54 includes a front wheel turning simulation operating device and a brake simulation operating device, which are connected to the flight control system 1 through sensors.
On the basis of the simulated aircraft steering simulation subsystem 5, the auxiliary steering system 54 is further limited to comprise a front wheel steering simulation steering device and a braking simulation steering device, so that the conditions of steering, braking and the like of the aircraft can be simulated, and more real experience is provided for trainers.
In order to further optimize the above technical solution, it is further defined that the sensor is connected to the flight control system 1 through a signal processing circuit on the basis of the above embodiment.
In order to further optimize the above technical solution, on the basis of the above embodiment, the signal processing circuit is further defined to include: a filter circuit, an amplifier circuit, an analog-to-digital conversion circuit, and a level adjustment circuit, which are shown in fig. 6 and fig. 7.
The force information, the displacement information and the rotation angle information collected by the sensor are transmitted to the flight control system 1 sequentially through the filter circuit, the amplifying circuit, the analog-to-digital conversion circuit and the level conditioning circuit. The level conditioning circuit consists of a photoelectric conversion module U1 and resistors R1 and R5, wherein R1 is a current-limiting resistor and is connected with a light-emitting tube in U1 in series, and R5 is an output resistor.
The signal processing circuit provided by the invention can output a stable level state, and the safety control effect of the aircraft control simulation system is ensured.
Claims (8)
1. A simulated aircraft control system, comprising: the system comprises a flight control system, a motion simulation subsystem, a visual simulation subsystem, a sound simulation subsystem, a manipulation simulation subsystem, a boarding simulation subsystem and an instructor console;
the flight control system is used for receiving and analyzing signals from the manipulation simulation subsystem and signals from the instructor console to obtain control instructions of each simulation subsystem and outputting the control instructions to each simulation subsystem;
each simulation subsystem receives respective control instruction to execute corresponding instruction;
the teacher control console is used for power control, aircraft state monitoring and setting simulation, environment control, fault setting and training course setting during training.
2. The simulated aircraft control system of claim 1, further comprising: an evaluation system coupled to the instructor console;
the evaluation system is used for receiving flight data of the simulated aircraft, storing the flight data into the database, and comparing and operating the flight data with parameters stored in the standard database in advance to obtain an evaluation result; and storing the evaluation result in the database, and sending the evaluation result to the instructor console for reference and calling by an instructor.
3. The simulated aircraft control system of claim 1, further comprising: the downloading module is connected with the instructor console;
the downloading module is used for downloading flight data of the simulation training according to the input personnel information.
4. A simulated aircraft control system as claimed in claim 1 wherein said maneuver simulation subsystem comprises: the aerobridge comprises a aerobridge operating lever, a rudder, a force servo actuating mechanism and an auxiliary operating system;
the boarding bridge operating rod is used for operating a boarding bridge;
the rudder is connected to the force servo actuator through a transmission mechanism, and a sensor is mounted on the transmission mechanism; the sensor is used for acquiring force information applied to the rudder, generated displacement information and rotation angle information;
the boarding bridge operating lever, the rudder, the force servo actuating mechanism and the auxiliary operating system are all connected with the flight control system.
5. A simulated aircraft control system as claimed in claim 4 wherein said boarding simulation subsystem comprises: the boarding control system comprises a boarding controller, an alarm lamp, an upper sensor and a lower sensor; the boarding controller is connected with the flight control system;
the alarm lamp, the upper sensor and the lower sensor are all connected with the boarding controller;
the boarding controller is used for controlling the boarding bridge to take off and land based on the boarding bridge joystick;
the alarm lamp is used for indicating the state of the boarding bridge;
the upper sensor is used for detecting the highest position of the boarding bridge;
the lower sensor is used for detecting the lowest position of the boarding bridge.
6. A simulated aircraft control system as claimed in claim 4 wherein said auxiliary operating system comprises a nose wheel steering simulated operator and a brake simulated operator, both connected to said flight control system by sensors.
7. A simulated aircraft control system as claimed in claim 4 wherein said sensors are connected to said flight control system by signal processing circuitry.
8. A simulated aircraft control system as claimed in claim 7 wherein said signal processing circuitry comprises: the device comprises a filter circuit, an amplifying circuit, an analog-to-digital conversion circuit and a level conditioning circuit;
the force information, the displacement information and the rotation angle information collected by the sensor are transmitted to the flight control system through the filter circuit, the amplifying circuit, the analog-to-digital conversion circuit and the level conditioning circuit in sequence.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202010010526.3A CN110992767A (en) | 2020-01-06 | 2020-01-06 | Simulated aircraft control system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202010010526.3A CN110992767A (en) | 2020-01-06 | 2020-01-06 | Simulated aircraft control system |
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| CN110992767A true CN110992767A (en) | 2020-04-10 |
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Citations (6)
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| CN103871292A (en) * | 2014-03-27 | 2014-06-18 | 芜湖航飞科技股份有限公司 | Full-function flight simulator |
| CN205485399U (en) * | 2016-02-05 | 2016-08-17 | 西安飞豹科技发展公司 | Flight simulator connecting bridge controlling means |
| KR20190072747A (en) * | 2017-12-18 | 2019-06-26 | (주)아레스 | Simulator system for emergency escape training of pilot by using parachute |
| CN209103578U (en) * | 2018-04-29 | 2019-07-12 | 北京摩诘创新科技股份有限公司 | A kind of instructor console of flight simulator |
| CN110444078A (en) * | 2019-08-26 | 2019-11-12 | 中仿智能科技（上海）股份有限公司 | A kind of control load system of simulated flight device |
| CN212694638U (en) * | 2020-07-29 | 2021-03-12 | 中国人民解放军91658部队 | Training plane flight and command simulator data exchange system |
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2020
- 2020-01-06 CN CN202010010526.3A patent/CN110992767A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103871292A (en) * | 2014-03-27 | 2014-06-18 | 芜湖航飞科技股份有限公司 | Full-function flight simulator |
| CN205485399U (en) * | 2016-02-05 | 2016-08-17 | 西安飞豹科技发展公司 | Flight simulator connecting bridge controlling means |
| KR20190072747A (en) * | 2017-12-18 | 2019-06-26 | (주)아레스 | Simulator system for emergency escape training of pilot by using parachute |
| CN209103578U (en) * | 2018-04-29 | 2019-07-12 | 北京摩诘创新科技股份有限公司 | A kind of instructor console of flight simulator |
| CN110444078A (en) * | 2019-08-26 | 2019-11-12 | 中仿智能科技（上海）股份有限公司 | A kind of control load system of simulated flight device |
| CN212694638U (en) * | 2020-07-29 | 2021-03-12 | 中国人民解放军91658部队 | Training plane flight and command simulator data exchange system |
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