NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Optimization of structure and control systemThe objective of this study is the simultaneous design of the structural and control system for space structures. This study is focused on considering the effect of the number and the location of the actuators on the minimum weight of the structure, and the total work done by the actuators for specified constraints and disturbance. The controls approach used is the linear quadratic regulator theory with constant feedback. At the beginning collocated actuators and sensors are provided in all the elements. The actuator doing the least work is removed one at a time, and the structure is optimized for the specified constraints on the closed-loop eigenvalues and the damping parameters. The procedure of eliminating an actuator is continued until an acceptable design satisfying the constraints is obtained. The study draws some conclusions on the trade between the total work done by the actuators, and the optimum weight and the number of actuators.
Document ID
19890015852
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Khot, N. S.
(Air Force Wright Aeronautical Labs. Wright-Patterson AFB, OH., United States)
Grandhi, Ramana V.
(Wright State Univ. Dayton, OH., United States)
Date Acquired
September 6, 2013
Publication Date
April 1, 1989
Publication Information
Publication: NASA. Langley Research Center, Recent Advances in Multidisciplinary Analysis and Optimization, Part 3
Subject Category
Aircraft Design, Testing And Performance
Accession Number
89N25223
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available