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A method for developing K/S boundary conditionsA method for developing the missing general K/S (Kustaanheimo/Stiefel) boundary conditions is presented, with use of the formalism of optimal control theory. As illustrative examples, the method is applied to the transfer between two position and velocity vectors and to the K/S Lambert problem to derive the missing terminal conditions. The necessary equations for a solution are then developed to the K/S Lambert problem with both the fictitious time, s, and the generalized eccentric anomaly, E, as the independent variables. The latter formulation, requiring the solution of only one nonlinear, well-behaved equation in one unknown, E, results in considerable simplification of the problem. This simplification is possible because the energy equation, in the E-formulation, is separable.
Document ID
19760057982
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Jezewski, D. J.
(NASA Johnson Space Center Mission Planning and Analysis Div., Houston, Tex., United States)
Date Acquired
August 8, 2013
Publication Date
March 1, 1976
Publication Information
Publication: Journal of the Astronautical Sciences
Volume: 24
Subject Category
Astronomy
Accession Number
76A40948
Distribution Limits
Public
Copyright
Other

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