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Linear statistical analysis of maneuver optimization techniquesIt is shown how a method for maneuver design during the Jovian satellite tour phase of the Galileo mission requires a full-scale redesign of the tour at each maneuver. Software was developed to provide insight into the statistical properties of this process; it is based on the use of linear perturbations to provide trajectory propagation and a least squares representation of the optimization. The result is a Monte Carlo program, making it possible to evaluate the proposed strategy.
Document ID
19890025311
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Maize, Earl H.
(California Institute of Technology Jet Propulsion Laboratory, Pasadena, United States)
Date Acquired
August 13, 2013
Publication Date
January 1, 1988
Subject Category
Astrodynamics
Report/Patent Number
AAS PAPER 87-486
Report Number: AAS PAPER 87-486
Meeting Information
Meeting: AAS/AIAA Astrodynamics Conference
Location: Kalispell, MT
Country: United States
Start Date: December 6, 1987
End Date: December 9, 1987
Sponsors: AIAA, AAS
Accession Number
89A12682
Distribution Limits
Public
Copyright
Other

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