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Feedback Control for Spacecraft Rendezvous and Docking

  • Published:1999-07 Issue:4 Volume:22 Page:609-611
  • ISSN:0731-5090
  • Container-title:Journal of Guidance, Control, and Dynamics
  • language:en
  • Short-container-title:Journal of Guidance, Control, and Dynamics

Author:

Kluever Craig A.1

Affiliation:

1. University of Missouri–Columbia, Kansas City, Missouri 64110-2499

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Applied Mathematics,Electrical and Electronic Engineering,Space and Planetary Science,Aerospace Engineering,Control and Systems Engineering

Cited by 55 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. Exact output tracking in prescribed finite time via funnel control;Automatica;2024-12

2. Orbit Rendezvous Maneuvers in Cislunar Space via Nonlinear Hybrid Predictive Control;Dynamics;2024-08-02

3. Control strategy for trading off solar power and control input while rendezvous and docking;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2024-06-03

4. Exact-Time Convergent Spacecraft Rendezvous using Sliding Mode Control;AIAA SCITECH 2024 Forum;2024-01-04

5. Adaptive Control of the Relative Position for Space Vehicles in the Rendezvous Missions;2023 27th International Conference on System Theory, Control and Computing (ICSTCC);2023-10-11
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