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Cross-platform extendible satellite dynamic simulation test system

A dynamic simulation and testing system technology, applied in general control systems, control/regulation systems, instruments, etc., can solve problems such as poor scalability of source code portability, easy to update and maintain, reduce complexity, and reduce costs Effect

Inactive Publication Date: 2012-02-15
BEIHANG UNIV
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Problems solved by technology

Therefore, the scalability of the system and the portability of source code are relatively poor

Method used

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  • Cross-platform extendible satellite dynamic simulation test system
  • Cross-platform extendible satellite dynamic simulation test system
  • Cross-platform extendible satellite dynamic simulation test system

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Experimental program
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Embodiment Construction

[0032] Such as figure 1 As shown, the system mainly includes three parts: satellite system simulator 1, flight environment and motion simulator 2, and operation monitoring and management system simulator 3. Satellite system simulator 1 is further divided into satellite attitude control system simulator 11 and satellite Fundamental Subsystem Simulator 12. Wherein, the flight environment and motion simulator 2 is composed of an environment simulator 21 and an orbit and attitude dynamics solver 22, which is used to simulate the satellite flight environment and flight dynamics process; the satellite attitude control system simulator 11 is used to simulate the satellite's Attitude control loop, including controller simulator 111, sensor simulator 112, and actuator simulator 113; satellite basic subsystem simulator 12, including power supply subsystem simulator 121 and telemetry remote control subsystem simulator 122; operation monitoring and management System 3 simulates the funct...

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Abstract

The invention discloses a cross-platform extendible satellite dynamic simulation test system, which comprises a satellite attitude control system simulator, a flight environment and motion simulator, a satellite basic subsystem simulator and an operation monitoring and management system simulator. The satellite attitude control system simulator comprises a sensor simulator, a controller simulatorand an actuating mechanism simulator; the flight environment and motion simulator comprises an orbit and attitude dynamics resolver, a celestial body simulator, a kinematics and dynamics turntable, akinematics and dynamics translation platform, a hot vacuum and electromagnetic environment simulator and the like; and the satellite basic subsystem simulator comprises a power supply subsystem simulator and a remote measuring and remote control subsystem simulator. The operation monitoring and management system simulates functions of a satellite ground measurement and control center, such as remote measuring data decoding, remote control command generating, data archiving and analyzing and operation managing. The cross-platform extendible satellite dynamic simulation test system has strong extendibility, can be conveniently transplanted on a development and debugging platform, a distributed real-time simulation platform and an embedded semi-physical real-time simulation platform.

Description

technical field [0001] The invention relates to a satellite dynamic simulation test system, in particular to a cross-platform scalable satellite dynamic simulation test system. Background technique [0002] Aerospace engineering has the characteristics of hugeness, complexity and high comprehensiveness. Before the satellite goes into space, it needs to do full component testing and system simulation, so as to check the design scheme and existing problems of the system. With the deepening of space exploration, there are more and more types and styles of satellites, and there have been multi-satellite space missions, such as formation flight, rendezvous and docking, inter-satellite detection and tracking, and inter-satellite on-orbit module replacement and filling. The existing attitude control simulation test system for a single type of single satellite can no longer meet the demand. [0003] The existing full-physical simulation and semi-physical simulation satellite attitu...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G05B17/02
Inventor 董云峰赵文冯建军黎岳鹏
Owner BEIHANG UNIV
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