PDF(310 KB)
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 & Complexity ›› 2022, Vol. 35 ›› Issue (2) : 688-702.
PDF(310 KB)
PDF(310 KB)
Fully-Actuated System Approach Based Optimal Attitude Tracking Control of Rigid Spacecraft with Actuator Saturation
| {{custom_ref.label}} |
{{custom_citation.content}}
{{custom_citation.annotation}}
|
/
| 〈 |
|
〉 |