Please use this identifier to cite or link to this item: https://hdl.handle.net/10356/96705
Title: Time-optimal reorientation for rigid satellite with reaction wheels
Authors: Zhou, Hao
Wang, Danwei
Wu, Baolin
Poh, Eng Kee
Keywords: DRNTU::Engineering::Electrical and electronic engineering
Issue Date: 2012
Source: Zhou, H., Wang, D., Wu, B., & Poh, E. K. (2012). Time-optimal reorientation for rigid satellite with reaction wheels. International Journal of Control, 85(10), 1452-1463.
Series/Report no.: International journal of control
Abstract: This article introduces a time-optimal reorientation manoeuvre controller with saturation constraints on both reaction wheels’ torques and angular momentum. The proposed control scheme consists of two parts. The first part is an open-loop time-minimum reorientation trajectory generated by the Legendre pseudospectral method. Actuator dynamics, saturations on control torques and angular momentums of reaction wheels are taken into account in generating the open-loop optimal trajectory. The second part is a closed-loop tracking control law to track the optimised reference trajectory based on attitude error dynamics with reaction wheel dynamics. Numerical simulations show that reaction wheel dynamics play an important role in attitude manoeuvres. The proposed controller performs better for rest-to-rest reorientation manoeuvre than other existing methods.
URI: https://hdl.handle.net/10356/96705
http://hdl.handle.net/10220/11587
ISSN: 0020-7179
DOI: 10.1080/00207179.2012.688873
Rights: © 2012 Taylor & Francis.
Fulltext Permission: none
Fulltext Availability: No Fulltext
Appears in Collections:EEE Journal Articles

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