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中国科学院数学与系统科学研究院期刊网
Electronic ISSN 1559-7067 Print ISSN 1009-6124
CN 11-4543/O1
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中文
Fully-Actuated System Approach Based Optimal Attitude Tracking Control of Rigid Spacecraft with Actuator Saturation
LIU Gaoqi, ZHANG Kai, LI Bin
Journal of Systems Science and Complexity . 2022, (
2
): 688 -702 . DOI: 10.1007/s11424-022-1515-8
