Fast Terminal Sliding Mode Control of Underactuated Spacecraft Formation Reconfiguration-Reference-Cited by-同舟云学术

Fast Terminal Sliding Mode Control of Underactuated Spacecraft Formation Reconfiguration

Published:2016-09 Issue:5 Volume:29 Page:04016020
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Huang Xu¹,Yan Ye²,Zhou Yang³,Hao Daoliang⁴

Affiliation:

1. Ph.D. Student, College of Aerospace Science and Engineering, National Univ. of Defense Technology, Changsha 410073, People’s Republic of China (corresponding author).

2. Professor, College of Aerospace Science and Engineering, National Univ. of Defense Technology, Changsha 410073, People’s Republic of China.

3. Ph.D. Student, College of Aerospace Science and Engineering, National Univ. of Defense Technology, Changsha 410073, People’s Republic of China.

4. Assistant Engineer, Luoyang Electronic Equipment Test Center, Luoyang 471003, People’s Republic of 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.1943-5525.0000610

Reference28 articles.

1. On ultimate boundedness control of uncertain systems in the absence of matching assumptions

2. Modeling and Analysis of Relative Hovering Control for Spacecraft

3. Non-singular terminal sliding mode control of rigid manipulators

4. A unified framework for the numerical solution of optimal control problems using pseudospectral methods

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