Necessary conditions for singular arcs for general restricted multi-body problem
We analyze the optimality of intermediate thrust arcs (singular arcs) of a rocket trajectory subject to multiple gravitational bodies in the restricted multi-body problem. We derive a series of necessary conditions for optimality including the generalized Legendre-Clebsch condition, and an explicit...
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Published in | 49th IEEE Conference on Decision and Control (CDC) pp. 5816 - 5821 |
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Main Authors | , , , |
Format | Conference Proceeding |
Language | English |
Published |
IEEE
01.12.2010
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Subjects | |
Online Access | Get full text |
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Summary: | We analyze the optimality of intermediate thrust arcs (singular arcs) of a rocket trajectory subject to multiple gravitational bodies in the restricted multi-body problem. We derive a series of necessary conditions for optimality including the generalized Legendre-Clebsch condition, and an explicit formula for the singular optimal control law. Our derivations become identical to Lawden's classical result if the equations of motion are reduced for a central gravity field. As a means to illustrate the practical nature of our results, we apply them to a Moon-Earth transfer problem and show that the extremal solution is bang-singular-bang. |
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ISBN: | 142447745X 9781424477456 |
ISSN: | 0191-2216 |
DOI: | 10.1109/CDC.2010.5717305 |