Adaptive Finite-Time Control for Attitude Tracking of Rigid Spacecraft
Author:
Affiliation:
1. Ph.D. Student, Institute of Control Engineering, Xi’an Jiaotong Univ., Xi’an 710049, China.
2. Professor, Institute of Control Engineering, Xi’an Jiaotong Univ., Xi’an 710049, China (corresponding author).
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.1943-5525.0000597
Reference35 articles.
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4. Bhat S. P. and Bernstein D. S. (1997). “Finite-time stability of homogeneous systems.” Proc. American Control Conf. Vol. 4 IEEE Albuquerque NM 2513–2514.
5. Sliding-mode controller design for spacecraft attitude tracking maneuvers
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