Integrated Geometric Optimal Control of Spacecraft Attitude and Orbit Based on SE(3)

Zhongzhong Zheng, Wei Shang, Jia Ai, Zou Yuhan, Zhou Liu. Integrated Geometric Optimal Control of Spacecraft Attitude and Orbit Based on SE(3). IEEE Access, 11:27382-27394, 2023. [doi]

Possibly Related Publications

The following publications are possibly variants of this publication: