TY - GEN
T1 - Gain-scheduled control for an antenna with multiple collocated sensors and actuators
AU - Lang, Xiaoyu
AU - Damaren, Christopher J.
N1 - Publisher Copyright:
© 2018, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
PY - 2018/1/1
Y1 - 2018/1/1
N2 - An output-based gain-scheduled controller is proposed for attitude maneuvers and vibration suppression in repurposing a large antenna. All sensor outputs are used as the gain-scheduled signals to maintain passivity of the antenna with multiple collocated actu- ators. Applying these special gain-scheduled signals permits the use of a strictly passive controller which degenerates to a scalar transfer function. As a result, the computational cost decreases dramatically. System stability can be guaranteed by using the passivity theorem along with the Kalman-Yakubovich-Popov (KYP) Lemma. Numerical simulation results are given to make a comparison between the proposed gain-scheduled control and a non-scheduled control scheme. In addition, an optimal form of the scheduling signals is found to minimize vertical displacements on the rim of the antenna, attitude errors, and control effort so as to give good performance.
AB - An output-based gain-scheduled controller is proposed for attitude maneuvers and vibration suppression in repurposing a large antenna. All sensor outputs are used as the gain-scheduled signals to maintain passivity of the antenna with multiple collocated actu- ators. Applying these special gain-scheduled signals permits the use of a strictly passive controller which degenerates to a scalar transfer function. As a result, the computational cost decreases dramatically. System stability can be guaranteed by using the passivity theorem along with the Kalman-Yakubovich-Popov (KYP) Lemma. Numerical simulation results are given to make a comparison between the proposed gain-scheduled control and a non-scheduled control scheme. In addition, an optimal form of the scheduling signals is found to minimize vertical displacements on the rim of the antenna, attitude errors, and control effort so as to give good performance.
UR - http://www.scopus.com/inward/record.url?scp=85141569718&partnerID=8YFLogxK
U2 - 10.2514/6.2018-0858
DO - 10.2514/6.2018-0858
M3 - Conference contribution
AN - SCOPUS:85141569718
SN - 9781624105265
T3 - AIAA Guidance, Navigation, and Control Conference, 2018
BT - AIAA Guidance, Navigation, and Control
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - AIAA Guidance, Navigation, and Control Conference, 2018
Y2 - 8 January 2018 through 12 January 2018
ER -