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Robust Neighboring Optimal Guidance for the Advanced Launch SystemIn recent years, optimization has become an engineering tool through the availability of numerous successful nonlinear programming codes. Optimal control problems are converted into parameter optimization (nonlinear programming) problems by assuming the control to be piecewise linear, making the unknowns the nodes or junction points of the linear control segments. Once the optimal piecewise linear control (suboptimal) control is known, a guidance law for operating near the suboptimal path is the neighboring optimal piecewise linear control (neighboring suboptimal control). Research conducted under this grant has been directed toward the investigation of neighboring suboptimal control as a guidance scheme for an advanced launch system.
Document ID
19930012820
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Hull, David G.
(Texas Univ. Austin, TX, United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1993
Subject Category
Launch Vehicles And Space Vehicles
Report/Patent Number
NASA-CR-192087
NAS 1.26:192087
Report Number: NASA-CR-192087
Report Number: NAS 1.26:192087
Accession Number
93N22009
Funding Number(s)
CONTRACT_GRANT: NAG1-944
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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