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Three-parameter tunable Tilt-Integral-Derivative (TID) controllerA feedback control system compensator of the PID type is provided, wherein the proportional component of the compensator is replaced with a tilted component having a transfer function s to the power of -1/n. The resulting transfer function of the entire compensator more closely approximates an optimal transfer function, thereby achieving improved feedback controller. Further, as compared to conventional PID compensators, the TID compensator allows for simpler tuning, better disturbance rejection ratio, and smaller effects of plant parameter variations on closed loop response.
Document ID
19950011898
Acquisition Source
Legacy CDMS
Document Type
Other - Patent
Authors
Lurie, Boris J.
(Jet Propulsion Lab. California Inst. of Tech., Pasadena, CA., United States)
Date Acquired
August 16, 2013
Publication Date
December 6, 1994
Subject Category
Cybernetics
Report/Patent Number
Patent Application Number: US-PATENT-APPL-SN-023253
Patent Number: US-PATENT-5,371,670
Patent Number: NASA-CASE-NPO-18492-1-CU
Accession Number
95N18313
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-PATENT-5,371,670|NASA-CASE-NPO-18492-1-CU
Patent Application
US-PATENT-APPL-SN-023253
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