Spacecraft attitude control by combination of various torquers-Reference-Cited by-同舟云学术

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Spacecraft attitude control by combination of various torquers

Published:2009-10 Issue:10 Volume:40 Page:995-1008
ISSN:0020-7721
Container-title:International Journal of Systems Science
language:en
Short-container-title:International Journal of Systems Science

Author:

Leeghim Henzeh,Lee Dong-Hun,Bang Hyochoong,Lee Kyungwon

Publisher

Informa UK Limited

Subject

Computer Science Applications,Theoretical Computer Science,Control and Systems Engineering

Link

http://www.tandfonline.com/doi/pdf/10.1080/00207720902974587

Reference20 articles.

1. Steering law design for redundant single-gimbal control moment gyroscopes

2. Singular Direction Avoidance Steering for Control-Moment Gyros

3. Junkins, JL and Kim, Y. 1993.Introduction to Dynamics and Control of Flexible Structures, AIAA, 9–64. Washington, DC: AIAA Inc.

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3. A control allocation approach for hybrid actuators;Fast Satellite Attitude Maneuver and Control;2022

4. Finite Time and Cooperative Control of Flight Vehicles;Advances in Industrial Control;2019

5. Angular Rate and Alignment Estimation for Gyroless Spacecraft by Only Star Trackers;International Journal of Control, Automation and Systems;2018-09-13

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