Dynamic Scaling–Based Noncertainty-Equivalent Adaptive Spacecraft Attitude Tracking Control-Reference-Cited by-同舟云学术

Dynamic Scaling–Based Noncertainty-Equivalent Adaptive Spacecraft Attitude Tracking Control

Published:2018-03 Issue:2 Volume:31 Page:04017098
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Wen Haowei¹,Yue Xiaokui²,Yuan Jianping²

Affiliation:

1. Ph.D. Candidate, National Key Laboratory of Aerospace Flight Dynamics, Northwestern Polytechnical Univ., Xian 710072, P.R. China (corresponding author).

2. Professor, National Key Laboratory of Aerospace Flight Dynamics, Northwestern Polytechnical Univ., Xian 710072, P.R. 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.1943-5525.0000818

Reference36 articles.

1. Adaptive Asymptotic Tracking of Spacecraft Attitude Motion with Inertia Matrix Identification

2. Adaptive systems, lack of persistency of excitation and bursting phenomena

3. Failures of adaptive control theory and their resolution;Anderson B. D.;Commun. Inf. Syst.,2005

4. Stabilization of Uncertain Nonlinear Systems via Immersion and Invariance

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