On the Advantages and Limitations of Sliding Mode Control for Spacecraft-Reference-Cited by-同舟云学术

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On the Advantages and Limitations of Sliding Mode Control for Spacecraft

Published:2010-06-26 Issue: Volume: Page:
ISSN:
Container-title:AIAA SPACE 2010 Conference & Exposition
language:
Short-container-title:

Author:

Ghosh Dastidar Rajarshi¹

Affiliation:

1. Massachusetts Institute of Technology

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2010-8777

Reference7 articles.

1. Nonlinear decoupling sliding mode control and attitude control of spacecraft

2. 5“AStudyofLinearvs.NonlinearTechniquesfortheReconfigurationofSatelliteFormations”,D.J.IrvineJr.,AirForceInstituteofTechnology, DepartmentofAeronauticsandAstronautics,Ph.DThesis,2001.

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. Robotic Manipulation and Capture in Space: A Survey;Frontiers in Robotics and AI;2021-07-19

2. Sliding-Mode Control Strategies for Rendezvous and Docking Maneuvers;Journal of Guidance, Control, and Dynamics;2017-06

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