Sub-optimal fixed-finite-horizon spacecraft configuration control on SE(3)
Author:
Funder
TUM University Foundation
Publisher
Elsevier BV
Subject
Mechanical Engineering,Aerospace Engineering
Reference42 articles.
1. Adaptive fault-tolerant attitude tracking control for spacecraft with time-varying inertia uncertainties;Hu;Chin J Aeronaut,2019
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3. Spacecraft formation-containment flying control with time-varying translational velocity;Chen;Chin J Aeronaut,2020
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Cited by 2 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
1. Fully-actuated-system-approach-based Attitude-orbit Integrated Control for Spacecraft Formation Flying;2023 2nd Conference on Fully Actuated System Theory and Applications (CFASTA);2023-07-14
2. Integrated Geometric Optimal Control of Spacecraft Attitude and Orbit Based on SE(3);IEEE Access;2023
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