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Method for simulating operating force feeling of helicopter by means of double force sources

A helicopter and dual force source technology, applied in simulators, educational appliances, simulation devices of space navigation conditions, etc., can solve the problems of influence fidelity, force simulation fidelity limitation, etc., and achieve convenient and logical modeling. Consistent, easy-to-achieve effects

Active Publication Date: 2014-04-30
长春天钛仿真科技有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Usually, one method is to use the original steering gear for the force loading simulation of the parallel channel, and the series channel has no loading force source, so that the inertial force, friction force and damping force of the serial channel and the fault state generated by the simulation need to be removed Force cannot be simulated, seriously affecting the fidelity of force sense
Another method is to use the simulation part as the loading force source. Due to the error in the modeling of the loading force and the difference in the physical characteristics of the simulation part and the original steering gear, the fidelity of the force simulation is also limited to a certain extent.

Method used

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  • Method for simulating operating force feeling of helicopter by means of double force sources
  • Method for simulating operating force feeling of helicopter by means of double force sources
  • Method for simulating operating force feeling of helicopter by means of double force sources

Examples

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Embodiment 1

[0037] Example 1 The method of using dual force sources to simulate the feeling of helicopter control force, the device used is composed as follows : The 1000M Ethernet 2 is respectively connected with the main flight simulation computer 1, the control load computer 3, the instructor console computer 4 and the autopilot computer 5; the RS485 data converter 7 is respectively connected with the control load computer 3 and the dsPIC single-chip microcomputer 9; the dsPIC single-chip microcomputer 9 Also be connected with photoelectric encoder 6, steering gear servo amplifier 8, electromagnetic force servo amplifier 10 respectively; Electromagnetic force servo amplifier 10 is connected with electromagnetic force servo loader 11; Electromagnetic force servo loader 11 is connected with driving stick 13; Original parallel rudder Machine 12 is connected with driving rod 13 and steering gear servo amplifier 8 respectively; Photoelectric encoder 6 is connected with driving rod 13 and ...

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Abstract

The invention provides a method for simulating operating force feeling of a helicopter by means of double force sources. A device used in the method forms a double loop control system simulating a parallel connection channel and a series connection channel of the helicopter. A steering gear serves as a force loading source for achieving the parallel connection channel of an operating system of the helicopter so as to complete force feeling simulation of the parallel connection channel; an electromagnetic force servo loading system serves as a force loading source of the series connection channel to achieve force feeling simulation of the series connection channel. An operating load system of the helicopter is comprehensively simulated through the double force loading sources, the operating force feeling of pilots is almost the same as that of a real plane, and naturalness of a flight simulator is improved. The parallel connection channel and the series connection channel are respectively controlled, and cross linking coupling does not exist; the parallel connection channel is identical to a control logical relationship of an original plane; the simulation force property of the series connection channel is known and modeling is convenient to achieve. Besides the fact that the device can simulate operations of the operating load system under automatic and manual driving conditions, the device can ensure that operating force feeling of other functions of the operating system is identical with that of a real helicopter.

Description

technical field [0001] The invention relates to a method for simulating the control force feeling of a helicopter by adopting dual force sources. Background technique [0002] The control load system is one of the important systems of the helicopter flight simulator. Usually, one method is to use the original steering gear for the force loading simulation of the parallel channel, and the series channel has no loading force source, so that the inertial force, friction force and damping force of the serial channel and the fault state generated by the simulation need to be removed The force cannot be simulated, which seriously affects the fidelity of the sense of force. Another method is to use the simulation part as the loading force source. Due to the error in the modeling of the loading force and the difference in the physical characteristics of the simulation part and the original steering gear, the fidelity of the force simulation is also limited to a certain extent. Co...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G09B9/46G09B9/28
Inventor 卢颖孙方义侯宇航赵建川韩志鹏
Owner 长春天钛仿真科技有限公司
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