Adaptive Finite-Time Control for Attitude Tracking of Spacecraft under Input Saturation-Reference-Cited by-同舟云学术

Adaptive Finite-Time Control for Attitude Tracking of Spacecraft under Input Saturation

Author:

Guo Yong¹,Huang Bing²,Wang Shuo³,Li Ai-jun⁴,Wang Chang-qing⁵

Affiliation:

1. Assistant Professor, School of Automation, Northwestern Polytechnical Univ., Xi’an, Shaanxi 710072, China (corresponding author).

2. Ph.D. Student, School of Automation, Northwestern Polytechnical Univ., Xi’an, Shaanxi 710072, China.

3. Engineer, Beijing Institute of Astronautical Systems Engineering, Beijing 100076, China.

4. Professor, School of Automation, Northwestern Polytechnical Univ., Xi’an, Shaanxi 710072, China.

5. Associate Professor, School of Automation, Northwestern Polytechnical Univ., Xi’an, Shaanxi 710072, China.

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Link

Reference22 articles.

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