TY - GEN
T1 - The application of error quaternion and PID control method in earth observation satellite's attitude control system
AU - Wang, Qiyu
AU - Yuan, Jianping
AU - Zhu, Zhanxia
PY - 2006
Y1 - 2006
N2 - Because of its payload's work characteristic, it requires much higher precision in earth observation satellite's attitude control systems than others. Most earth observation satellites use zero-momentum three-axis stabilization control method. This paper investigates this control method in satellite control system, deducing the dynamics and kinematics of satellite attitude's model expressed by attitude error quaternion, applying PID control method in this model, and then simulating and evaluating the method preliminarily. The results show that the method can achieve the require precision quickly.
AB - Because of its payload's work characteristic, it requires much higher precision in earth observation satellite's attitude control systems than others. Most earth observation satellites use zero-momentum three-axis stabilization control method. This paper investigates this control method in satellite control system, deducing the dynamics and kinematics of satellite attitude's model expressed by attitude error quaternion, applying PID control method in this model, and then simulating and evaluating the method preliminarily. The results show that the method can achieve the require precision quickly.
UR - http://www.scopus.com/inward/record.url?scp=33750961458&partnerID=8YFLogxK
M3 - 会议稿件
AN - SCOPUS:33750961458
SN - 0780393953
SN - 9780780393950
T3 - 1st International Symposium on Systems and Control in Aerospace and Astronautics
SP - 128
EP - 131
BT - 1st International Symposium on Systems and Control in Aerospace and Astronautics
T2 - 1st International Symposium on Systems and Control in Aerospace and Astronautics
Y2 - 19 January 2006 through 21 January 2006
ER -