A flight control system test result evaluation method

A technology of flight control system and test results, applied in the field of aviation, can solve problems such as unscientific, large random differences in evaluation, inaccurate evaluation results, etc., and achieve good results and simple matching algorithms

Pending Publication Date: 2019-05-03
XIAN AIRCRAFT DESIGN INST OF AVIATION IND OF CHINA
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  • Claims
  • Application Information

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Problems solved by technology

[0003] On the one hand, the intuitive evaluation of the above test results is affected by the subjective will of the test personnel such as engineering experience and theoretical level. On the other hand, only individual feature points are used to judge, resulting in large random differences in evaluation. , different experimenters often come to different conclusions

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  • A flight control system test result evaluation method
  • A flight control system test result evaluation method
  • A flight control system test result evaluation method

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Embodiment Construction

[0027] In order to make the purpose, technical solutions and advantages of the embodiments of the present invention more clear, the technical solutions in the embodiments of the present invention will be clearly and completely described below in conjunction with the drawings in the embodiments of the present invention. Apparently, the described embodiments are some, not all, embodiments of the present invention. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts belong to the protection scope of the present invention.

[0028]The features of various aspects of the embodiments of the present invention will be described in detail below. In the following detailed description, numerous specific details are set forth in order to provide a thorough understanding of the present invention. It will be apparent, however, to one skilled in the art that the present invention may be prac...

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Abstract

The invention provides a flight control system test result evaluation method. The method comprises the following steps: synchronously applying a test excitation signal to a tested flight control system and a flight control system simulation model; recording a response output signal of the tested flight control system, and recording a response output signal of the simulation model; After performingdata smoothing or digital filtering on the response output signal of the tested flight control system, solving the spatial distance of the response output signal of the tested flight control system and the response output signal of the simulation model at the same data point; judging the matching between the response output signal of the tested flight control system and the response output signalof the simulation model; and evaluating the test result of the flight control system according to the judgment result. The method can achieve the automatic evaluation of the test result of the flightcontrol system, is accurate in evaluation result, and is high in practicability.

Description

technical field [0001] The invention relates to the technical field of aviation, in particular to a method for evaluating test results of a flight control system. Background technique [0002] In the design and development of flight control systems, it is often necessary to carry out tests at different levels, such as component-level, subsystem-level, sub-system-level and even system-level testing and verification tests, to test the functions and performance of the designed product and its component systems Whether it meets the design requirements. Such as flight control system control law transmission ratio test, time domain response test, frequency domain response test, etc. In the above tests, by applying different excitation signals to the input end of the flight control system under test, the output response of the system under test is measured and recorded. Signal, generate the graphic curve of the system output response signal, and then the test personnel analyze the...

Claims

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Application Information

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IPC IPC(8): G06F17/50
CPCY02T90/00
Inventor 支超有江飞鸿张龑
Owner XIAN AIRCRAFT DESIGN INST OF AVIATION IND OF CHINA
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