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Integrated tools for control-system analysisThe basic functions embedded within a user friendly software package (MATRIXx) are used to provide a high level systems approach to the analysis of linear control systems. Various control system analysis configurations are assembled automatically to minimize the amount of work by the user. Interactive decision making is incorporated via menu options and at selected points, such as in the plotting section, by inputting data. There are five evaluations such as the singular value robustness test, singular value loop transfer frequency response, Bode frequency response, steady-state covariance analysis, and closed-loop eigenvalues. Another section describes time response simulations. A time response for random white noise disturbance is available. The configurations and key equations used for each type of analysis, the restrictions that apply, the type of data required, and an example problem are described. One approach for integrating the design and analysis tools is also presented.
Document ID
19890009938
Acquisition Source
Legacy CDMS
Document Type
Technical Publication (TP)
Authors
Ostroff, Aaron J.
(PRC Systems Services Co. Hampton, VA., United States)
Proffitt, Melissa S.
(NASA Langley Research Center Hampton, VA, United States)
Clark, David R.
(Planning Research Corp. Hampton, VA., United States)
Date Acquired
September 5, 2013
Publication Date
March 1, 1989
Publication Information
Publisher: NASA
Subject Category
Aircraft Stability And Control
Report/Patent Number
NAS 1.60:2885
NASA-TP-2885
L-16482
Report Number: NAS 1.60:2885
Report Number: NASA-TP-2885
Report Number: L-16482
Accession Number
89N19309
Funding Number(s)
PROJECT: RTOP 505-66-01-02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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