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Manual Attitude Control of the Lunar Module
Robert F. Stengel
Charles Stark Draper Laboratory, Massachusetts Institute of Technology, Cambridge, Mass. -
Handling Qualities for Pilot Control of Apollo Lunar-Landing Spacecraft
Donald C. Cheatham and Clarke T. Hackler
NASA Manned Spacecraft Center, Houston, Texas -
Quaternion Feedback Control for Rigid-Body Spacecraft
Hans-Christian B. Jensen, Rafal Wisniewski
Department of Control Engineering, Institute of Electronic Systems, Aalborg University, 9220 Aalborg O�, Denmark -
The Attitude Control Problem
John Ting-Yung Wen, Member, IEEE, and Kenneth Kreutz-Delgado, Member, IEEE -
Robust Attitude Stabilization of Spacecraft Using Nonlinear Quaternion Feedback
S. M. Joshi, A. G. Kelkar, and J. T.-Y. Wen -
Quaternion Feedback Attitude Control Design: A Nonlinear H∞ Approach
Long-Life Show, Jyh-Ching Juang, Ying-Wen Jan, and Chen-Tzung Lin -
Satellite Attitude Control by Quaternion-Based Backstepping
Raymond Kristiansen* and Per J. Nicklasson**
Department of Computer Science, Electrical Engineering and Space technology
Narvik University College
8515 Narvik, Norway -
Optimal Spacecraft Terminal Attitude Control Synthesis
by the Quaternion Method
M. V. Levskii*
Space System Research and Development Institute,
Khrunichev State Research and Production Space Center,
Tikhonravova 27, Yubileynii, Moscow oblast, 141091 Russia -
Nonlinear Attitude Control for a Rigid Spacecraft
by Feedback Linearization
Hyochoong Bang† · Jung-Shin Lee * · Youn-Ju Eun**
Division of Aerospace Engineering, KAIST
373-1, Kusong-Dong, Yousong-Gu, Daejon, 305-701
Created
April 9, 2012 18:33
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Attitude Control
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