Fully-Actuated System Approach Based Optimal Attitude Tracking Control of Rigid Spacecraft with Actuator Saturation

Gaoqi Liu, Kai Zhang, Bin Li. Fully-Actuated System Approach Based Optimal Attitude Tracking Control of Rigid Spacecraft with Actuator Saturation. J. Systems Science & Complexity, 35(2):688-702, 2022. [doi]

Abstract

Abstract is missing.