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Developments toward Active Control of Space Structures
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English
Abstract
Satisfactory performance of some recent and near-future spacecraft requires precise pointing and a stationary structural configuration. Elements of modern control theory and structural-dynamics technology are being combined to help achieve these objectives. This paper reviews some analytical and experimental research undertaken to develop methods for actively controlling flexible space structures.
Authors
Citation
Stroud, R., Hamma, G., Smith, S., and Lyons, M., "Developments toward Active Control of Space Structures," SAE Technical Paper 801234, 1980, https://doi.org/10.4271/801234.Also In
References
- Stroud R. C. Bonner C. J. Chambers G. J. “Modal-Testing Options For Spacecraft Development” SAE Paper No. 781043 SAE Aerospace Meeting Nov 1978
- Herzberg R. J. Johansen K. Stroud R. C. “Dynamics and Control of Flexible Satellites” AIAA/ASME Structures, Structural Dynamics, and Materials Conference Bethesda, MD April 1978
- “Seminar on Understanding Digital Control and Analysis in Vibration Testing” Shock and Vibration Information Center May 1975
- Hamma G. A. Smith S. Stroud R. C. “Simulation of Dynamic Loads by Multi-Channel Digital Control” AIAA/ASME Structures, Structural Dynamics and Materials Conference Bethesda, MD April 1978
- Stroud R. C. Smith S. Hamma G. A. “Digital Control of Dynamic-Response Histories” Joint Conference of Acoustical Society of America and Acoustical Society of Japan Honolulu, Hawaii Dec 1978
- Smith S. Stroud R. C. Hamma G. A. Johnson L. “Digital-Control Techniques for a Three-Axis Vibration-Testing System” SAE Paper No. 801233 1980 SAE Aerospace Congress and Exposition Los Angeles, California 13 October 1980
- Aubrun J. N. Gupta N. K. “Control of Large Space Structures: An integrated Approach” AIAA Guidance and control Conference Aug 1979
- Aubrun J. N. Gupta N. K. et. al. “Stability Augmentation for Flexible Space Structures” IEEE Conference on Decision and Control Ft. Lauderdale Dec 1979
- Stroud R. C. Smith S. Hamma G. A. “MODALAB - A New System for Structural Dynamic Testing” 46th Shock and Vibration Symposium 22-25 October 1975 Shock and Vibration Bulletin No. 46, Part 5 153 175 August 1976