Novel Adaptive Saturated Attitude Tracking Control of Rigid Spacecraft with Guaranteed Transient and Steady-State Performance-Reference-Cited by-同舟云学术

Novel Adaptive Saturated Attitude Tracking Control of Rigid Spacecraft with Guaranteed Transient and Steady-State Performance

Published:2018-09 Issue:5 Volume:31 Page:04018062
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Yin Zeyang¹,Luo Jianjun²,Wei Caisheng¹

Affiliation:

1. Ph.D. Student, National Key Laboratory of Aerospace Flight Dynamics, School of Astronautics, Northwestern Polytechnical Univ., Youyi West St., Beilin District, Xi’an, Shaanxi 710072, China.

2. Professor, National Key Laboratory of Aerospace Flight Dynamics, School of Astronautics, Northwestern Polytechnical Univ., Youyi West St., Beilin District, Xi’an, Shaanxi 710072, 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.1943-5525.0000884

Reference53 articles.

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

2. Discrete-Time Nonlinear HJB Solution Using Approximate Dynamic Programming: Convergence Proof

3. Dynamics and control of dual-spin gyrostat spacecraft with changing structure

4. Galerkin approximations of the generalized Hamilton-Jacobi-Bellman equation

5. Guaranteeing prescribed performance and contact maintenance via an approximation free robot force/position controller

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