Bounded Finite-Time Coordinated Attitude Control via Output Feedback for Spacecraft Formation-Reference-Cited by-同舟云学术

Bounded Finite-Time Coordinated Attitude Control via Output Feedback for Spacecraft Formation

Published:2015-09 Issue:5 Volume:28 Page:04014129
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Hu Qinglei¹,Zhang Jian²

Affiliation:

1. Professor, Dept. of Control Science and Engineering, Harbin Institute of Technology, No. 92, West Da-zhi St., Harbin 150001, China (corresponding author).

2. Ph.D. Student, Dept. of Control Science and Engineering, Harbin Institute of Technology, No. 92, West Da-zhi St., Harbin 150001, 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.1943-5525.0000468

Reference36 articles.

1. Abdessameud A. and Tayebi A. (2008). “Decentralized attitude alignment control of spacecraft within a formation without angular velocity measurements.” Proc. Int. Federation of Automatic Control (IFAC) World Congress Elsevier Amsterdam Netherlands 1766–1771.

2. Attitude Synchronization of a Group of Spacecraft Without Velocity Measurements

3. Backstepping Control Design with Actuator Torque Bound for Spacecraft Attitude Maneuver

4. Rigid body attitude coordination without inertial frame information

5. Finite-Time Stability of Continuous Autonomous Systems

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