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On-orbit closed loop verification system for satellite control system

A satellite control system and verification system technology, applied in the field of on-orbit closed-loop verification system of satellite control system, can solve problems such as incomplete composition of closed-loop control system, improve the authenticity of on-orbit verification, save verification cost, reduce verification risk and cost effect

Active Publication Date: 2015-04-29
BEIJING INST OF CONTROL ENG
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  • Summary
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  • Application Information

AI Technical Summary

Problems solved by technology

Since no real actuators are used, no control forces and moments are applied to real satellites, only real sensors and controllers are tested, so it is incomplete as a closed-loop control system

Method used

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  • On-orbit closed loop verification system for satellite control system
  • On-orbit closed loop verification system for satellite control system
  • On-orbit closed loop verification system for satellite control system

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Embodiment Construction

[0018] Below in conjunction with accompanying drawing and specific embodiment the present invention is described in further detail:

[0019] The virtual dynamics and kinematics module is run in the aerospace control computer, and the module performs the dynamics and kinematics calculation of the satellite, and the specific parameters can be flexibly designed according to the purpose of the test. Such as kinematic equation:

[0020] q · 1 q · 2 q · 3 q · 4 = 1 2 ...

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PUM

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Abstract

The invention discloses an on-orbit closed loop verification system for a satellite control system. The on-orbit closed loop verification system is suitable for on-orbit verification on new technology and products of the satellite control system. Close loop work conditions for the new technology or products to be applied to the satellite control system are established by running a satellite dynamics and kinematics calculation module, an executing mechanism control force or torque calculation module and a sensor measured value calculation module in a control computer. By the adoption of the on-orbit closed loop verification system, under the condition of lack of an executing mechanism, a sensor and even a controlled object, on-orbit real-time closed loop verification on new technology and products of the satellite control system can be achieved, and the authenticity of on-orbit verification on the new technology and the new products is remarkably improved.

Description

technical field [0001] The invention relates to an on-orbit closed-loop verification system of a satellite control system, in particular to an on-orbit closed-loop verification system of an incomplete satellite control system, which is suitable for on-orbit test verification of new technologies and products of the satellite control system. Background technique [0002] For a long time, the on-orbit test of new products (real sensors) of the satellite control system has adopted an open-loop verification system, such as figure 1 , that is, the verification and assessment of product performance and functions is carried out by transmitting the working information and status of the product in orbit through telemetry, and there is a lack of closed-loop verification and assessment. This is mainly due to the high cost of satellites and the high requirements for reliability. New products generally adopt the method of carrying for the first on-orbit verification. That is to say, the...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G05B23/02
CPCG05B23/02
Inventor 于萍张洪华王鹏基王华强杨巍杨洁
Owner BEIJING INST OF CONTROL ENG
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