Flight quality semi-physical simulation test method

A semi-physical simulation, flight quality technology, applied in the field of flight quality semi-physical simulation test, to reduce uncertain factors, reduce development risks, and speed up development progress

Inactive Publication Date: 2018-04-20
CHINA HELICOPTER RES & DEV INST
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  • Description
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Problems solved by technology

At present, there is no relevant flight quality semi-physical simulation test technology in the field of helicopters in China, so a flight control system flight quality semi-physical simulation technology is needed to ensure that the performance indicators of the helicopter meet the technical requirements

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Embodiment Construction

[0024] In order to make the objectives, technical solutions and advantages of the present invention clearer, the technical solutions in the embodiments of the present invention will be described in more detail below in conjunction with the drawings in the embodiments of the present invention. In the drawings, the same or similar reference numerals denote the same or similar elements or elements having the same or similar functions throughout. The described embodiments are some, but not all, embodiments of the invention. The embodiments described below by referring to the figures are exemplary and are intended to explain the present invention and should not be construed as limiting the present invention. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without creative efforts fall within the protection scope of the present invention. Embodiments of the present invention will be described in detail below ...

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Abstract

The invention discloses a flight quality semi-physical simulation test method, and belongs to the technical field of flight control. The flight quality semi-physical simulation test method comprises the steps that one, a simulation management system accepts an attitude response signal from a flight control system, performs dynamic mathematic model calculation and sends a calculation result to a bus signal simulation system, the bus signal simulation system converts the calculation result into a bus simulation signal and transmits the bus simulation signal to the flight control system, and theflight control system performs a corresponding attitude response according to the collected bus simulation signal and transmits the attitude response to the simulation management system; two, flight quality semi-physical simulation test units are formulated; three, a flight quality semi-physical simulation test is performed in allusion to the established simulation test units, and signal parameters of each test unit are observed and recorded at the same time; and four, a data analysis and quality assessment system performs grade assessment on each test unit according to the signal parameters of each test unit. The flight quality semi-physical simulation test method shortens the argumentation process of model development, reduces uncertain factors in the development process and acceleratesthe development progress.

Description

technical field [0001] The invention belongs to the technical field of flight control, and in particular relates to a flight quality semi-physical simulation test method. Background technique [0002] The function and performance of the flight control system directly affect the overall performance index and flight safety of the helicopter, so the flight control system needs to be fully and fully tested and verified on the ground, and the semi-physical simulation of the flight quality of the flight control system is the core of it component. At present, there is no relevant flight quality semi-physical simulation test technology in the field of helicopters in China, so a flight control system flight quality semi-physical simulation technology is needed to ensure that the performance indicators of the helicopter meet the technical requirements. Contents of the invention [0003] Purpose of the present invention: in order to solve the above problems, the present invention pr...

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G05B17/02
CPCG05B17/02
Inventor 廖枫黄丹
Owner CHINA HELICOPTER RES & DEV INST
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