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Design of state-feedback controllers including sensitivity reduction, with applications to precision pointingThe design procedure of feedback controllers was described and the considerations for the selection of the design parameters were given. The frequency domain properties of single-input single-output systems using state feedback controllers are analyzed, and desirable phase and gain margin properties are demonstrated. Special consideration is given to the design of controllers for tracking systems, especially those designed to track polynomial commands. As an example, a controller was designed for a tracking telescope with a polynomial tracking requirement and some special features such as actuator saturation and multiple measurements, one of which is sampled. The resulting system has a tracking performance comparing favorably with a much more complicated digital aided tracker. The parameter sensitivity reduction was treated by considering the variable parameters as random variables. A performance index is defined as a weighted sum of the state and control convariances that sum from both the random system disturbances and the parameter uncertainties, and is minimized numerically by adjusting a set of free parameters.
Document ID
19760012134
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Hadass, Z.
(Stanford Univ. CA, United States)
Date Acquired
September 3, 2013
Publication Date
August 1, 1974
Subject Category
Spacecraft Instrumentation
Report/Patent Number
NASA-CR-146437
SUDAAR-482
Report Number: NASA-CR-146437
Report Number: SUDAAR-482
Accession Number
76N19222
Funding Number(s)
CONTRACT_GRANT: NGR-05-020-019
CONTRACT_GRANT: F33615-72-C-1297
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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