"Fully-Actuated System Approach Based Optimal Attitude Tracking Control of ..."

Gaoqi Liu, Kai Zhang, Bin Li (2022)

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DOI: 10.1007/S11424-022-1515-8

access: closed

type: Journal Article

metadata version: 2024-08-07

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Gaoqi Liu, Kai Zhang, Bin Li:
Fully-Actuated System Approach Based Optimal Attitude Tracking Control of Rigid Spacecraft with Actuator Saturation. J. Syst. Sci. Complex. 35(2): 688-702 (2022)

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