TY - GEN
T1 - Attitude tracking control using recursive passivation technique
AU - Xi, Boqi
AU - Yi, Guoxing
AU - Shen, Bochang
PY - 2006
Y1 - 2006
N2 - The main problem addressed is the attitude tracking control of a rigid satellite. A nonlinear feedback control scheme is presented, based on recursive passivation through backstepping. The control structure designed consists of PID-like feedback plus some feedforward terms, which achieves enhancing the tracking performance by compensating for the plant dynamics. Quaternion attitude representation, which is four-parameter and void of singularity when compared with other three-parameter representations, such as Euler angle, is adopted to finish our main control formulation. Simulation results are included to demonstrate the effectiveness of the proposed control technique.
AB - The main problem addressed is the attitude tracking control of a rigid satellite. A nonlinear feedback control scheme is presented, based on recursive passivation through backstepping. The control structure designed consists of PID-like feedback plus some feedforward terms, which achieves enhancing the tracking performance by compensating for the plant dynamics. Quaternion attitude representation, which is four-parameter and void of singularity when compared with other three-parameter representations, such as Euler angle, is adopted to finish our main control formulation. Simulation results are included to demonstrate the effectiveness of the proposed control technique.
UR - https://www.scopus.com/pages/publications/33750948630
M3 - 会议稿件
AN - SCOPUS:33750948630
SN - 0780393953
SN - 9780780393950
T3 - 1st International Symposium on Systems and Control in Aerospace and Astronautics
SP - 404
EP - 407
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 -