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Helicopter control load simulation system and method

A helicopter and load technology, applied in the field of flight simulation, can solve problems such as overloading of data processing ports

Pending Publication Date: 2022-06-24
佛山智壹科技有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] The main purpose of the present invention is to provide a helicopter control load simulation system and method, aiming at solving the technical problem of overloading of the data processing port of the control module of the control load in the existing helicopter control load simulation system

Method used

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  • Helicopter control load simulation system and method

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Experimental program
Comparison scheme
Effect test

Embodiment 1

[0063] refer to figure 1 , the present invention provides a first embodiment of a helicopter manipulation load simulation system, figure 1 It is a structural diagram of the first embodiment of a helicopter manipulation load simulation system of the present invention.

[0064] This embodiment provides a helicopter manipulation load simulation system, the system includes a main simulation module, a manipulation load control module, a signal distribution module, a drive module and an execution module;

[0065] The main simulation module is connected with the manipulation load control module, and is used for providing model force to the manipulation load control module;

[0066] The manipulation load control module is connected with the signal distribution module for generating an initial control signal according to the model force and the received loading force and angle values, and sending the initial control signal to the signal distribution module;

[0067] The signal distri...

Embodiment 2

[0075] refer to figure 1 , based on the above-mentioned first embodiment, the drive module includes a longitudinal drive unit, a lateral drive unit, a collective drive unit and a pedal drive unit;

[0076] The longitudinal drive unit is connected with the signal distribution module, and is used for generating longitudinal control instructions according to the target control signal, and sending the longitudinal control instructions to the execution module;

[0077] The lateral drive unit is connected with the signal distribution module, and is used for generating lateral control instructions according to the target control signal, and sending the lateral control instructions to the execution module;

[0078] The collective pitch drive unit is connected with the signal distribution module, and is used for generating collective pitch control instructions according to the target control signal, and sending the collective pitch control instructions to the execution module;

[0079...

Embodiment 3

[0085] refer to figure 1 , based on the second embodiment above, the execution module includes a longitudinal execution unit, a lateral execution unit, a collective pitch execution unit and a pedal execution unit;

[0086] The longitudinal execution unit is connected with the longitudinal drive unit, and is used to control the longitudinal movement of the simulation platform in the horizontal direction according to the longitudinal control instruction;

[0087] The lateral execution unit is connected with the lateral drive unit, and is used to control the lateral movement of the simulation platform in the horizontal direction according to the lateral control instruction;

[0088] The collective pitch execution unit is connected with the collective pitch drive unit, and is used to control the simulation platform to move in the direction perpendicular to the horizontal direction according to the collective pitch control instruction;

[0089] The pedal execution unit is connecte...

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Abstract

The invention discloses a helicopter control load simulation system and method, and relates to the technical field of flight simulation, the system comprises a main simulation module, a control load control module, a signal distribution module, a driving module and an execution module; the main simulation module is connected with the control load control module and provides model force; the control load control module is connected with the signal distribution module, generates an initial control signal according to the model force and the received loading force and angle value, and sends the initial control signal to the signal distribution module; the signal distribution module is connected with the driving module, integrates the initial control signals to obtain target control signals, and sends the target control signals to the driving module; the driving module is connected with the execution module, generates a control instruction according to the target control signal, and sends the control instruction to the execution module; and the execution module controls a simulation platform of the helicopter to move according to the control instruction. Through the signal distribution module, the technical problem that the load of the data processing port of the control load control module is too heavy is solved.

Description

technical field [0001] The invention relates to the technical field of flight simulation, in particular to a helicopter manipulation load simulation system and method. Background technique [0002] Helicopter handling load simulation system is one of the key systems of helicopter special situation simulation, which is used to simulate the flight control system of helicopter. Its performance directly affects the handling quality of helicopter special situation simulation. [0003] In the related art, the handling load control module in the helicopter handling load simulation system is directly connected with the driving module, so that the handling load control module directly performs data processing with the driving module of the helicopter simulation platform, and at this time, the data processing port of the handling load control module is loaded. It is too heavy, and at the same time manipulates the two-way processing of data between the load control module and the drive...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G05B17/02
CPCG05B17/02
Inventor 徐厚超冯韬李宜平
Owner 佛山智壹科技有限公司
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