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Title: |
Optimal control of large space structures via generalized inverse matrix
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Author(s): |
Nguyen, Charles C.; Fang, Xiaowen
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Abstract: |
Independent Modal Space Control (IMSC) is a control scheme that decouples the space structure into n independent second-order subsystems according to n controlled modes and controls each mode independently. It is well-known that the IMSC eliminates control and observation spillover caused when the conventional coupled modal control scheme is employed. The independent control of each mode requires that the number of actuators be equal to the number of modelled modes, which is very high for a faithful modeling of large space structures. A control scheme is proposed that allows one to use a reduced number of actuators to control all modeled modes suboptimally. In particular, the method of generalized inverse matrices is employed to implement the actuators such that the eigenvalues of the closed-loop system are as closed as possible to those specified by the optimal IMSC. Computer simulation of the proposed control scheme on a simply supported beam is given.
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NASA Center: |
NASA (non Center Specific)
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Publication Date: |
JAN 1, 1987
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Document Source: |
CASI |
Online Source: |
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Document ID: |
19880004525
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Accession ID: |
88N13907
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Publication Information: |
Number of Pages = 5 |
Report Number: |
NAS 1.26:182336; NASA-CR-182336
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Contract-Grant-Task Number: |
NAG5-949 |
Price Code: |
A01 |
Keywords: |
BEAMS (SUPPORTS); COMPUTERIZED SIMULATION; LARGE SPACE STRUCTURES; MATHEMATICAL MODELS; MATRICES (MATHEMATICS); SPACECRAFT CONTROL; FEEDBACK CONTROL; OPTIMAL CONTROL; STATE ESTIMATION; STATE VECTORS;
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Accessibility: |
Unclassified; No Copyright; Unlimited; Publicly available; |
Updated/Added to NTRS: |
2005-08-25 |
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