Statistical linearization for multi-input/multi-output nonlinearities
Author:
Affiliation:
1. National Chiao-Tung University, Hsinchu, Taiwan,Republic of China
2. NASA Ames Research Center, Moffett Field,California 94035
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Applied Mathematics,Electrical and Electronic Engineering,Space and Planetary Science,Aerospace Engineering,Control and Systems Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.20791
Reference19 articles.
1. Optimal feedback slewing of flexible spacecraft
2. Planar, time-optimal, rest-to-rest slewing maneuvers of flexible spacecraft
3. Quaternion feedback for spacecraft large angle maneuvers
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