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
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;
Conference_Titel :
Control & Automation (ICCA), 11th IEEE International Conference on
Conference_Location :
Taichung
DOI :
10.1109/ICCA.2014.6871014