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Statistics of Delta v magnitude for a trajectory correction maneuver containing deterministic and random componentsA number of interplanetary missions now being planned involve placing deterministic maneuvers along the flight path to alter the trajectory. Lee and Boain (1973) examined the statistics of trajectory correction maneuver (TCM) magnitude with no deterministic ('bias') component. The Delta v vector magnitude statistics were generated for several values of random Delta v standard deviations using expansions in terms of infinite hypergeometric series. The present investigation uses a different technique (Monte Carlo simulation) to generate Delta v magnitude statistics for a wider selection of random Delta v standard deviations and also extends the analysis to the case of nonzero deterministic Delta v's. These Delta v magnitude statistics are plotted parametrically. The plots are useful in assisting the analyst in quickly answering questions about the statistics of Delta v magnitude for single TCM's consisting of both a deterministic and a random component. The plots provide quick insight into the nature of the Delta v magnitude distribution for the TCM.
Document ID
19820056470
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Bollman, W. E.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Chadwick, C.
(California Institute of Technology, Jet Propulsion Laboratory, Navigation Systems Section, Pasadena CA, United States)
Date Acquired
August 10, 2013
Publication Date
August 1, 1982
Subject Category
Astrodynamics
Report/Patent Number
AIAA PAPER 82-1429
Meeting Information
Meeting: Astrodynamics Conference
Location: San Diego, CA
Start Date: August 9, 1982
End Date: August 11, 1982
Sponsors: American Institute of Aeronautics and Astronautics and American Astronautical Society
Accession Number
82A40005
Distribution Limits
Public
Copyright
Other

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