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An analytic approach to two-fixed-impulse transfers between Keplerian orbitsSolutions are obtained for the two-impulse transfer of a vehicle between arbitrary inclined orbits in an inverse-square force field with the restriction that the magnitude of each of the two impulses has a fixed preassigned value. The two magnitudes need not be equal. The equations for the conservation of angular momentum and energy are augmented by the Laplace integral; these equations establish linear relationships between several of the variables. This set of linear equations and one of two quadratic equations constitute the analytically tractable part of the solution. The remaining part, consisting of finding the zeros (if they exist) of a single trigonometric function of one variable, is solved using numerical methods. Explicit lower bounds on each of the magnitudes of the two impulses are obtained by requiring the solution be real. Graphical results are presented to illustrate the solution.
Document ID
19820060943
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Jezewski, D. J.
(NASA Johnson Space Center Houston, TX, United States)
Mittleman, D.
(Oberlin College Oberlin, OH, United States)
Date Acquired
August 10, 2013
Publication Date
October 1, 1982
Subject Category
Astrodynamics
Accession Number
82A44478
Distribution Limits
Public
Copyright
Other

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