Attitude Coordinated Control for Docked Spacecraft Based on Estimated Coupling Torque-Reference-Cited by-同舟云学术

Attitude Coordinated Control for Docked Spacecraft Based on Estimated Coupling Torque

Published:2016-11 Issue:6 Volume:29 Page:04016058
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Huang Panfeng¹,Wang Ming²,Meng Zhongjie³,Zhang Fan⁴,Liu Zhengxiong⁵

Affiliation:

1. Professor, National Key Laboratory of Aerospace Flight Dynamics, and Research Center for Intelligent Robotics, School of Astronautics, Northwestern Polytechnical Univ., Xi’an 710072, China (corresponding author).

2. Engineer, North Automatic Control Technology Institute, Taiyuan 030006, China.

3. Associate Professor, National Key Laboratory of Aerospace Flight Dynamics, and Research Center for Intelligent Robotics, School of Astronautics, Northwestern Polytechnical Univ., Xi’an 710072, China.

4. Ph.D. Candidate, National Key Laboratory of Aerospace Flight Dynamics, and Research Center for Intelligent Robotics, School of Astronautics, Northwestern Polytechnical Univ., Xi’an 710072, China.

5. Lecturer, National Key Laboratory of Aerospace Flight Dynamics, and Research Center for Intelligent Robotics, School of Astronautics, Northwestern Polytechnical Univ., Xi’an 710072, China.

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Link

http://ascelibrary.org/doi/pdf/10.1061/%28ASCE%29AS.1943-5525.0000645

Reference40 articles.

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2. Aghili F. (2009). “Optimal control of a space manipulator for detumbling of a satellite.” Int. Conf. on Robotics and Automation IEEE New York 3019–3024.

3. Experiments with model-simplified computed-torque manipulator controllers for free-flying robots

4. A review of space tether research

5. Sliding mode control using modified Rodrigues parameters

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