The determination of minimum-fuel or minimum-time space trajectories has been pursued for decades, using different methods of solution. This work illus-trates some symmetry properties that hold for optimal space trajectories and can considerably simplify their determination. The existence of symmetry prop-erties is demonstrated in the presence of certain boundary conditions for the problem of interest. If the linear Euler-Hill equations of motion are used, a pair of properties are proven to hold for minimum-time and minimum-fuel rendez-vous trajectories, both in two and in three dimensions. With regard to minimum-fuel paths, the primer vector theory predicts the existence of several powered phases, divided by coast arcs. In general, the optimal thrust sequence and dura-tion depend on the time evolution of the switching function, and can be proven to satisfy interesting symmetry properties, provided that a pair of elementary boundary conditions holds. In the context of the circular restricted three-body problem, the theorem of image trajectories, proven about 50 years ago, estab-lishes the symmetry properties of feasible trajectories. In this work this theorem is extended to optimal trajectories, thus substantiating a conjecture that dates back to the 60's

Symmetry properties of optimal space trajectories / Pontani, Mauro. - 153:(2015), pp. 1553-1572. ( 2nd International Academy of Astronautics Conference on Dynamics and Control of Space Systems, DyCoSS 2014 Rome, Italy 2014).

Symmetry properties of optimal space trajectories

PONTANI, MAURO
Primo
2015

Abstract

The determination of minimum-fuel or minimum-time space trajectories has been pursued for decades, using different methods of solution. This work illus-trates some symmetry properties that hold for optimal space trajectories and can considerably simplify their determination. The existence of symmetry prop-erties is demonstrated in the presence of certain boundary conditions for the problem of interest. If the linear Euler-Hill equations of motion are used, a pair of properties are proven to hold for minimum-time and minimum-fuel rendez-vous trajectories, both in two and in three dimensions. With regard to minimum-fuel paths, the primer vector theory predicts the existence of several powered phases, divided by coast arcs. In general, the optimal thrust sequence and dura-tion depend on the time evolution of the switching function, and can be proven to satisfy interesting symmetry properties, provided that a pair of elementary boundary conditions holds. In the context of the circular restricted three-body problem, the theorem of image trajectories, proven about 50 years ago, estab-lishes the symmetry properties of feasible trajectories. In this work this theorem is extended to optimal trajectories, thus substantiating a conjecture that dates back to the 60's
2015
2nd International Academy of Astronautics Conference on Dynamics and Control of Space Systems, DyCoSS 2014
aerospace engineering; space and planetary science;
04 Pubblicazione in atti di convegno::04b Atto di convegno in volume
Symmetry properties of optimal space trajectories / Pontani, Mauro. - 153:(2015), pp. 1553-1572. ( 2nd International Academy of Astronautics Conference on Dynamics and Control of Space Systems, DyCoSS 2014 Rome, Italy 2014).
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Utilizza questo identificativo per citare o creare un link a questo documento: https://hdl.handle.net/11573/959971
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