Structural modifications to reduce the LOS-error in large space structures
Author:
Affiliation:
1. USAF, Wright Aeronautical Laboratories,Wright-Patterson AFB, OH
2. Dayton, University, Dayton,OH
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1984-997
Reference7 articles.
1. 'Azzo,J. J., and Houpis, "Linear Control System Analysis and Design," 2nd Ed.McGraw-Hill, New York, 1981, pp.93-99.
2. Comparison of Optimality Criteria Algorithms for Minimum Weight Design of Structures
3. ALGORITHMS BASED ON OPTIMALITY CRITERIA TO DESIGN MINIMUM WEIGHT STRUCTURES
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1. On optimization of structural and control systems using a reduced order model;Structural Optimization;1990-09
2. Game theory approach for the integrated design of structures and controls;AIAA Journal;1988-04
3. Simultaneous structure/control optimization of large flexible spacecraft;28th Structures, Structural Dynamics and Materials Conference;1987-04-06
4. Optimum Control of Structures;Computer Aided Optimal Design: Structural and Mechanical Systems;1987
5. Optimal structural modifications to enhance the active vibration control of flexible structures;AIAA Journal;1986-08
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