Optimal control of a rigid body with dissimilar actuators
Author:
Affiliation:
1. NASA Langley Research Center, Hampton, Virginia 23681-0001
2. North Carolina State University, Raleigh, North Carolina 27695-7921
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/10.2514/3.21692
Reference10 articles.
1. Vibration Control Experiment of a Slewing Flexible Beam
2. Three Simple and Efficient Methods for Vibration Control of Slewing Flexible Structures
3. Robust time-optimal control - Frequency domain approach
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