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An Ensemble Averaging Approach to Optimal Guidance Polynomial ApproximationsAn approach to optimal guidance synthesis is developed in which an ensemble-averaged second order approximation to the performance function is minimized subject to constraints on the means and variances of other functions. The minimization is with respect to coefficients of assumed polynomial approximations of a linear feedback control law (in which the state is perfectly known) and coefficients in a linear termination law. A brief comparison is drawn with deterministic neighboring extremal control. While attention is directed mainly to first order necessary conditions, some comments are made on numerical solution by first and second order successive approximation methods. Extensions to include disturbances other than initial errors and to include state estimation errors are discussed briefly.
Document ID
19650023452
Acquisition Source
Marshall Space Flight Center
Document Type
Other - Technical Report
Authors
Henry J Kelley
(Analytical Mechanics Associates (United States) Hampton, United States)
Walter F Denham
(Analytical Mechanics Associates (United States) Hampton, United States)
Date Acquired
August 2, 2013
Publication Date
July 12, 1965
Publication Information
Publication: Progress Report No. 7 on Studies in the Fields of Space Flight and Guidance Theory
Publisher: National Aeronautics and Space Administration
Subject Category
Astrodynamics
Report/Patent Number
NASA-TM-X-53292
Accession Number
65N33053
Funding Number(s)
CONTRACT_GRANT: NAS8-11241
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
Approximation Method
Guidance
Polynomial
Optimal Control
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