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Sliding mode control method having terminal convergence in finite timeAn object of this invention is to provide robust nonlinear controllers for robotic operations in unstructured environments based upon a new class of closed loop sliding control methods, sometimes denoted terminal sliders, where the new class will enforce closed-loop control convergence to equilibrium in finite time. Improved performance results from the elimination of high frequency control switching previously employed for robustness to parametric uncertainties. Improved performance also results from the dependence of terminal slider stability upon the rate of change of uncertainties over the sliding surface rather than the magnitude of the uncertainty itself for robust control. Terminal sliding mode control also yields improved convergence where convergence time is finite and is to be controlled. A further object is to apply terminal sliders to robot manipulator control and benchmark performance with the traditional computed torque control method and provide for design of control parameters.
Document ID
19950012647
Acquisition Source
Legacy CDMS
Document Type
Other - Patent
Authors
Venkataraman, Subramanian T.
(Jet Propulsion Lab. California Inst. of Tech., Pasadena, CA., United States)
Gulati, Sandeep
(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-921192
Patent Number: US-PATENT-5,371,669
Patent Number: NASA-CASE-NPO-18584-1-CU
Accession Number
95N19062
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-PATENT-5,371,669|NASA-CASE-NPO-18584-1-CU
Patent Application
US-PATENT-APPL-SN-921192
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