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Simultaneous structural and control optimization via linear quadratic regulator eigenstructure assignment
- Source :
- NASA-Marshall Space Flight Center, The 58th Shock and Vibration Symposium, Volume 1
- Publication Year :
- 1987
- Publisher :
- United States: NASA Center for Aerospace Information (CASI), 1987.
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Abstract
- A method for simultaneous structural and control design of large flexible space structures (LFSS) to reduce vibration generated by disturbances is presented. Desired natural frequencies and damping ratios for the closed loop system are achieved by using a combination of linear quadratic regulator (LQR) synthesis and numerical optimization techniques. The state and control weighing matrices (Q and R) are expressed in terms of structural parameters such as mass and stiffness. The design parameters are selected by numerical optimization so as to minimize the weight of the structure and to achieve the desired closed-loop eigenvalues. An illustrative example of the design of a two bar truss is presented.
- Subjects :
- Structural Mechanics
Subjects
Details
- Language :
- English
- Database :
- NASA Technical Reports
- Journal :
- NASA-Marshall Space Flight Center, The 58th Shock and Vibration Symposium, Volume 1
- Publication Type :
- Report
- Accession number :
- edsnas.19880004240
- Document Type :
- Report