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A constrained optimal PID-like controller design for spacecraft attitude stabilization
Institution:1. Department of Control Science and Engineering, Harbin Institute of Technology, P.O. Box 327, Harbin 150001, China;2. Department of Mathematics and Statistics, Curtin University. GPO Box U1987, Perth WA 6845, Australia;3. Center for Control Theory and Guidance Technology, Harbin Institute of Technology, 210, Building 2F, Technology Park, Harbin 150001, China;1. Institute for Systems Research, University of Maryland, College Park, United States;2. Astrome Technologies Pvt Ltd, Bangalore, India;3. Department of Computer Science and Automation, Indian Institute of Science, Bangalore, India;4. System Sciences and Automation, Indian Institute of Science, Bangalore, India
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