Adaptive Spacecraft Attitude Tracking and Parameter Estimation with Actuator Uncertainties-Reference-Cited by-同舟云学术

Adaptive Spacecraft Attitude Tracking and Parameter Estimation with Actuator Uncertainties

Published:2014-09 Issue:5 Volume:27 Page:04014022
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Jingrui Zhang¹,Jin Jin²,Zaozhen Liu³

Affiliation:

1. Professor, Key Laboratory of Dynamics and Control of Flight Vehicle, Ministry of Education, School of Aerospace Engineering, Beijing Institute of Technology, Beijing 100081, P.R. China (corresponding author).

2. Post-Doctor, School of Aerospace, Tsinghua Univ., Beijing 100083, P.R. China.

3. Professor, Key Laboratory of Dynamics and Control of Flight Vehicle, Ministry of Education, School of Aerospace Engineering, Beijing Institute of Technology, Beijing 100081, 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.1943-5525.0000317

Reference14 articles.

1. Controllability of Spacecraft Attitude Using Control Moment Gyroscopes

2. Error analysis and a new steering law design for spacecraft control system using SGCMGs

3. Jin L. and Xu S. J. (2008). “Study on attitude dynamics and control of spacecraft using angular momentum exchange devices.” Doctoral dissertation Beijing Univ. Beijing 96–101.

4. Kim D. MacKunis W. Fitz-Coy N. and Dixon W. E. (2009). “Precision IPACS in the presence of dynamic uncertainty.” Proc. Joint 48th IEEE Conf. on Decision and Control and 28th Chinese Control Conf. Institute of Electrical and Electronics Engineers (IEEE) New York 5959–5964.

5. Survey of Technology Developments in Flywheel Attitude Control and Energy Storage Systems

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