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Non-Causal Controller Approximation Methodology Augmented with Model Reference Control – Robust DesignThis paper describes the development of a new control design methodology based on a non-causal controller structure and its approximation. The non-causal controller design is based on a loop shaping approach. Partial fraction decomposition is used, along with derivative approximations, to derive a proper transfer function design for a causal control structure. The premise for this non-causal control methodology is that the phase delay as a function of frequency ideally remains within approximately -90o, which tends to make the system robustly stable to uncertainties in the plant dynamics. To have a predictable control system response in lieu of the tolerance of this methodology to relatively large uncertainty in the plant dynamics, the approach is augmented with model reference control. The addition of model reference control can potentially further enhance the robustness of the design. A control system design example is presented in this paper, along with simulation results, to demonstrate the high degree of robustness of this non-causal methodology and its augmentation.
Document ID
20210018453
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
George Kopasakis
(Glenn Research Center Cleveland, Ohio, United States)
Date Acquired
July 9, 2021
Publication Date
August 2, 2021
Subject Category
Aeronautics (General)
Report/Patent Number
E-19963
NASA/TM-20210018453
Funding Number(s)
WBS: 725017.02.03.02.04
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Technical Review
NASA Technical Management
Keywords
Control Systems
Feedback Control
Robust Control
Classical Control
Model Reference Control
Root Locus Control Design
Loop Shaping Control Design
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