Design and Simulation of satellite attitude control system based on Simulink

被引：0

作者：

Zhang, Yang ^{[1
]}

Gan, Qingbo ^{[1
]}

Kang, Jingshu ^{[2
]}

机构：

[1] Chinese Acad Sci, Space Syst Dept, Acad Optoelect, Beijing 100094, Peoples R China

[2] China Astronaut Publishing House, Beijing 100048, Peoples R China

来源：

SELECTED PAPERS OF THE PHOTOELECTRONIC TECHNOLOGY COMMITTEE CONFERENCES HELD NOVEMBER 2015 | 2016年 / 9796卷

关键词：

satellite attitude control; visual simulation; earth-oriented; virtual reality;

D O I：

10.1117/12.2230844

中图分类号：

TM [电工技术]; TN [电子技术、通信技术];

学科分类号：

0808 ; 0809 ;

摘要：

In order to research satellite attitude control system design and visual simulation, the simulation framework of satellite dynamics and attitude control using Simulink were established. The design of satellite earth-oriented control system based on quaternion feedback was completed. The 3D scene based on VR was created and models in the scene were driven by simulation data of Simulink. By coordinate transformation. successful observing the scene in inertial coordinate system, orbit coordinate system and body coordinate system. The result shows that application of simulation method of Simulink combined with VR in the design of satellite attitude control system field, has the advantages of high confidence level, hard real-time property, multi-perspective and multi-coordinate system observing the scene, and improves the comprehensibility and accuracy of the design.

引用

页数：7

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