Improved Adaptive Sliding Mode Control for Rigid Spacecraft Attitude Tracking-Reference-Cited by-同舟云学术

Improved Adaptive Sliding Mode Control for Rigid Spacecraft Attitude Tracking

Published:2014-07 Issue:4 Volume:27 Page:04014004
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Cong Binglong¹,Chen Zhen²,Liu Xiangdong³

Affiliation:

1. Engineer, Beijing Research Institute of Mechanical Equipment, Yongdinglu Rd. 50, Haidian District, Beijing 100854, China.

2. Lecturer, School of Automation, Beijing Institute of Technology, 5 South Zhongguancun St., Haidian District, Beijing 100081, China (corresponding author).

3. Professor, Key Laboratory for Intelligent Control and Decision of Complex Systems, School of Automation, 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.1943-5525.0000281

Reference24 articles.

1. Time-varying sliding modes for second-order systems

2. Robust Tracking Control Design for Spacecraft Under Control Input Saturation

3. A Nonlinear Disturbance Observer for Multivariable Systems and Its Application to Magnetic Bearing Systems

4. Sliding mode control using modified Rodrigues parameters

5. Variable structure control of nonlinear systems: a new approach

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