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Nonlinear system guidance in the presence of transmission zero dynamicsAn iterative procedure is proposed for computing the commanded state trajectories and controls that guide a possibly multiaxis, time-varying, nonlinear system with transmission zero dynamics through a given arbitrary sequence of control points. The procedure is initialized by the system inverse with the transmission zero effects nulled out. Then the 'steady state' solution of the perturbation model with the transmission zero dynamics intact is computed and used to correct the initial zero-free solution. Both time domain and frequency domain methods are presented for computing the steady state solutions of the possibly nonminimum phase transmission zero dynamics. The procedure is illustrated by means of linear and nonlinear examples.
Document ID
19950016387
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Meyer, G.
(NASA Ames Research Center Moffett Field, CA, United States)
Hunt, L. R.
(NASA Ames Research Center Moffett Field, CA, United States)
Su, R.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1995
Subject Category
Engineering (General)
Report/Patent Number
A-95014
NASA-TM-4661
NAS 1.15:4661
Report Number: A-95014
Report Number: NASA-TM-4661
Report Number: NAS 1.15:4661
Accession Number
95N22804
Funding Number(s)
PROJECT: RTOP 505-64-52
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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