TY - GEN
T1 - Induced L2 norm control for missile early-warning satellite attitude maneuver
AU - Zeng, Ming
AU - Wang, Jia
AU - Yu, Zhiwei
AU - Ma, Guangfu
AU - Wu, Zhipeng
PY - 2010
Y1 - 2010
N2 - In this paper, the Missile Early Warning Satellite Attitude Control problem is introduced, A two step incorporated and systematic method for modeling and control of missile early warning satellite is formulated. Firstly, the nonlinear dynamic and kinematics equation of the missile early warning satellite are reformulated to linear parameter variation (LPV) system. Secondly, based on the LPV model, an induced L2 norm controller is introduced to eliminate the affect caused by the rotation of onboard mobile facilities, the designed LPV controller can guarantee that the induced L2 norm from disturbance to attitude tracking error is less than a pre-given number. The LPV controller design problem is solved by Sum of Squares (SOS) programming techniques. The effectiveness of the proposed control technique is shown in simulations.
AB - In this paper, the Missile Early Warning Satellite Attitude Control problem is introduced, A two step incorporated and systematic method for modeling and control of missile early warning satellite is formulated. Firstly, the nonlinear dynamic and kinematics equation of the missile early warning satellite are reformulated to linear parameter variation (LPV) system. Secondly, based on the LPV model, an induced L2 norm controller is introduced to eliminate the affect caused by the rotation of onboard mobile facilities, the designed LPV controller can guarantee that the induced L2 norm from disturbance to attitude tracking error is less than a pre-given number. The LPV controller design problem is solved by Sum of Squares (SOS) programming techniques. The effectiveness of the proposed control technique is shown in simulations.
KW - Attitude control
KW - Induced L norm control
KW - Linear parameter variation(LPV)
KW - Missile early-warning satellite
KW - Mobile facilities
UR - https://www.scopus.com/pages/publications/79952127446
U2 - 10.1109/ISSCAA.2010.5632402
DO - 10.1109/ISSCAA.2010.5632402
M3 - 会议稿件
AN - SCOPUS:79952127446
SN - 9781424460441
T3 - ISSCAA2010 - 3rd International Symposium on Systems and Control in Aeronautics and Astronautics
SP - 610
EP - 615
BT - ISSCAA2010 - 3rd International Symposium on Systems and Control in Aeronautics and Astronautics
T2 - 3rd International Symposium on Systems and Control in Aeronautics and Astronautics, ISSCAA2010
Y2 - 8 June 2010 through 10 June 2010
ER -