中国科学院数学与系统科学研究院期刊网
JSSC
Fully-Actuated System Approach Based Optimal Attitude Tracking Control of Rigid Spacecraft with Actuator Saturation
LIU Gaoqi, ZHANG Kai, LI Bin
Fully-Actuated System Approach Based Optimal Attitude Tracking Control of Rigid Spacecraft with Actuator Saturation
LIU Gaoqi, ZHANG Kai, LI Bin
系统科学与复杂性 . 2022, (2): 688 -702 .  DOI: 10.1007/s11424-022-1515-8