"Attitude Trajectory Planning for Spacecraft With Time-Varying Mass Using ..."

Yueyang Liu, Qinglei Hu, Haoyang Yang (2024)

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DOI: 10.1109/TAES.2024.3439266

access: closed

type: Journal Article

metadata version: 2025-01-25

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Yueyang Liu, Qinglei Hu, Haoyang Yang:
Attitude Trajectory Planning for Spacecraft With Time-Varying Mass Using Sequential Conic Optimization. IEEE Trans. Aerosp. Electron. Syst. 60(6): 9045-9059 (2024)

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