Parameter Identification–Based Attitude Stabilization Control of Spacecraft with Multiaccessories during Orbital Maneuver-Reference-Cited by-同舟云学术

Parameter Identification–Based Attitude Stabilization Control of Spacecraft with Multiaccessories during Orbital Maneuver

Published:2017-05 Issue:3 Volume:30 Page:04016099
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Liu Xiangdong¹,Xin Xing²,Li Zhen³^ORCID,Sheng Yongzhi⁴,Chen Zhen⁵

Affiliation:

1. Professor, School of Automation and Chinese National Key Laboratory of Complex System Intelligent Control and Decision, Beijing Institute of Technology, Beijing 100081, China.

2. School of Automation, Beijing Institute of Technology, Beijing 100081, China; presently, Beijing Institute of Electronic System Engineering, Beijing 100854, China.

3. Associate Professor, School of Automation and Chinese National Key Laboratory of Complex System Intelligent Control and Decision, Beijing Institute of Technology, Beijing 100081, China (corresponding author). ORCID: .

4. Lecturer, School of Automation and Chinese National Key Laboratory of Complex System Intelligent Control and Decision, Beijing Institute of Technology, Beijing 100081, China.

5. Associate Professor, School of Automation and Chinese National Key Laboratory of Complex System Intelligent Control and Decision, Beijing Institute of Technology, Beijing 100081, 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.1943-5525.0000693

Reference40 articles.

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4. On the Computational Complexity of Peer-to-Peer Satellite Refueling Strategies

5. Dimitrov D. N. and Yoshida K. (2004). “Momentum distribution in a space manipulator for facilitating the post-impact control.” Proc. 2004 IEEE/RSJ Int. Conf. on Intelligent Robots and Systems 2004 (IROS 2004) Vol. 4 IEEE New York 3345–3350.

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