DocumentCode
1775437
Title
Research on modeling and simulation of satellite attitude control system
Author
Xiaoguang Hu ; Xiang Li
Author_Institution
Autom. Sci. & Electr. Eng., Beihang Univ., Beijing, China
fYear
2014
fDate
18-20 June 2014
Firstpage
744
Lastpage
749
Abstract
Satellite is a specific product with a 4-H characteristic: high-tech, high-cost, high-benefit and high-risk, which makes satellite difficult to develop. However, simulation technology has the potential to fix the problem. It is highly reliable, non-destructive and can be recycled regardless of the time and space. All the advantages enable the technology to provide an effective way to reduce the cost and risk of satellite production. The paper focuses on the modeling technology which is used for simulating satellite on-orbit performance and dynamic environment, thus it can provide a general simulation framework for test during the development of a satellite.
Keywords
aerospace simulation; artificial satellites; attitude control; cost reduction; risk management; vehicle dynamics; control system modeling; control system simulation; cost reduction; dynamic environment; modeling technology; risk reduction; satellite attitude control system; satellite development; satellite on-orbit performance simulation; satellite production; simulation technology; Attitude control; Equations; Mathematical model; Position measurement; Satellites; Sensors; Vectors;
fLanguage
English
Publisher
ieee
Conference_Titel
Control & Automation (ICCA), 11th IEEE International Conference on
Conference_Location
Taichung
Type
conf
DOI
10.1109/ICCA.2014.6871014
Filename
6871014
Link To Document