Attitude Control and Vibration Suppression for Flexible Spacecraft Using Control Moment Gyroscopes-Reference-Cited by-同舟云学术

Attitude Control and Vibration Suppression for Flexible Spacecraft Using Control Moment Gyroscopes

Published:2016-01 Issue:1 Volume:29 Page:04015027
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Hu Quan¹,Zhang Jingrui²

Affiliation:

1. Postdoctoral Research Fellow, School of Aerospace Engineering, Beijing Institute of Technology, Beijing 100081, People’s Republic of China (corresponding author).

2. Professor, School of Aerospace Engineering; Beijing Institute of Technology, Beijing 100081, People’s Republic of 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.1943-5525.0000513

Reference35 articles.

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4. Barkana I. (2008). “A modified invariance principle and gain convergence in adaptive control.” IEEE 25th Conventionof Electrical and Electronics Engineers in Israel (IEEE 2008) Eilat Israel 800–804.

5. Defending the beauty of the Invariance Principle

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