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A Higher-Order Sliding Mode Three-Axis Solar Pressure Satellite Attitude Control System

  • Published:2016-01 Issue:1 Volume:29 Page:04015019
  • ISSN:0893-1321
  • Container-title:Journal of Aerospace Engineering
  • language:en
  • Short-container-title:J. Aerosp. Eng.

Author:

Lee Keum W.1,Singh Sahjendra N.2

Affiliation:

1. Professor, Division of Electronic Information and Communication, Catholic Kwandong Univ., Gangwon 210-701, Republic of Korea.

2. Professor, Dept. of Electrical and Computer Engineering, Univ. of Nevada Las Vegas, Las Vegas, NV 89154-4026 (corresponding author).

Publisher

American Society of Civil Engineers (ASCE)

Subject

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

Cited by 12 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Robust non-aggressive three-axis attitude control of spacecraft: dynamic sliding mode approach;Control Theory and Technology;2023-11

2. Continuous Twisting Sliding Mode Control for Spacecraft Attitude Maneuver;2023 IEEE 12th International Conference on Communication Systems and Network Technologies (CSNT);2023-04-08

3. A third‐order sliding mode controller for nonlinear multivariable systems;Asian Journal of Control;2023-02-06

4. An output feedback back-stepping attitude control for rigid satellite;Transactions of the Institute of Measurement and Control;2023-02-01

5. Sliding Mode Attitude Control of Flexible Spacecraft with Rotational Components;Lecture Notes in Electrical Engineering;2023
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