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Flight control system simulation method and platform, server and storage medium

A technology of flight control system and simulation method, which is applied in the field of computer simulation, can solve the problems of inability to achieve simulation effects, long flight control system cycle, and low efficiency, and achieve the effects of reducing dependence, improving efficiency, and shortening cycle

Pending Publication Date: 2020-08-21
SHANGHAI KELIANG INFORMATION ENG
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AI Technical Summary

Problems solved by technology

[0003] However, the inventors have found that at least the following problems exist in the existing technology: the existing basic model can only perform offline simulation, and cannot achieve real-time simulation effects. It is necessary to continuously debug and correct according to the results of the test or test flight, resulting in a long cycle and low efficiency for the development of the flight control system

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  • Flight control system simulation method and platform, server and storage medium
  • Flight control system simulation method and platform, server and storage medium
  • Flight control system simulation method and platform, server and storage medium

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Embodiment Construction

[0027] In order to make the objectives, technical solutions and advantages of the present invention clearer, each embodiment of the present invention will be described in detail below with reference to the accompanying drawings. However, those of ordinary skill in the art can appreciate that, in the various embodiments of the present invention, many technical details are set forth in order for the reader to better understand the present application. However, even without these technical details and various changes and modifications based on the following embodiments, the technical solutions claimed in the present application can be realized.

[0028] The first embodiment of the present invention relates to a flight control system simulation method. By constructing N simulation models of the flight control system under test, and simulating the flight control system under test using the Linux platform according to the N simulation models, the tested flight control system can be s...

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Abstract

The embodiment of the invention relates to the field of computer simulation, and discloses a flight control system simulation method, which comprises the following steps: constructing N simulation models for verifying a tested flight control system, N being a positive integer; and simulating the tested flight control system by adopting a Linux platform according to the simulation model. The embodiment of the invention further provides a flight control system simulation platform, a server and a storage medium. According to the flight control system simulation method and platform, the server andthe storage medium provided by the embodiment of the invention, the period of developing the flight control system is shortened, and the efficiency is improved.

Description

technical field [0001] The invention relates to the field of computer simulation, in particular to a flight control system simulation method, platform, server and storage medium. Background technique [0002] The flight control system is an important part of the aircraft and the operating platform of the flight control algorithm. The flight control system controls the attitude of the aircraft to complete the flight tasks in various modes of the aircraft. In the process of developing the flight control system, the existing basic mode is to first complete the independent component development and offline operation of the algorithm model on the desktop. After the desktop simulation is completed, the semi-physical test and field test are carried out in combination with the real flight controller and aircraft prototype. It is the conventional discrete component test and the integrated test of the whole machine after the components are installed to complete the development of the...

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G06F30/20G06F30/15
CPCG06F30/20G06F30/15
Inventor 路国光曹文天邹毅军
Owner SHANGHAI KELIANG INFORMATION ENG
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