Automated generation and optimization of ballistic lunar capture transfer trajectories

Repository

Automated generation and optimization of ballistic lunar capture transfer trajectories

Show simple record

dc.contributor.advisor Ocampo, Cesar
dc.creator Griesemer, Paul Ricord
dc.date.accessioned 2009-10-26T16:18:05Z
dc.date.available 2009-10-26T16:18:05Z
dc.date.created 2009-08
dc.date.issued 2009-10-26T16:18:05Z
dc.identifier.uri http://hdl.handle.net/2152/6669
dc.description.abstract The successful completion of the Hiten mission in 1991 provided real-world validation of a class of trajectories defined as ballistic lunar capture transfers. This class of transfers is often considered for missions to the Moon and for tours of the moons of other planets. In this study, the dynamics of the three and four body problems are examined to better explain the mechanisms of low energy transfers in the Earth-Moon system, and to determine their optimality. Families of periodic orbits in the restricted Earth-Sun-spacecraft three body problem are shown to be generating families for low energy transfers between orbits of the Earth. The low energy orbit-to-orbit transfers are shown to require less fuel than optimal direct transfers between the same orbits in the Earth-Sun-spacecraft circular restricted three body problem. The low energy transfers are categorized based on their generating family and the number of flybys in the reference three body trajectory. The practical application of these generating families to spacecraft mission design is demonstrated through a robust nonlinear targeting algorithm for finding Sun-Earth- Moon-spacecraft four body transfers based on startup transfers indentified in the Earth- Sun three body problem. The local optimality of the transfers is examined through use of Lawden’s primer vector theory, and new conditions of optimality for single-impulse-to-capture lunar transfers are established.
dc.format.medium electronic
dc.language.iso eng
dc.rights Copyright © is held by the author. Presentation of this material on the Libraries' web site by University Libraries, The University of Texas at Austin was made possible under a limited license grant from the author who has retained all copyrights in the works.
dc.subject Hiten mission
dc.subject Trajectories
dc.subject Ballistic lunar capture transfers
dc.subject Moon missions
dc.subject Low energy transfers
dc.subject Lawden’s primer vector theory
dc.subject Orbit-to-orbit transfers
dc.subject Optimal direct transfers
dc.title Automated generation and optimization of ballistic lunar capture transfer trajectories
dc.description.department Aerospace Engineering and Engineering Mechanics
dc.type.genre Thesis
dc.type.material text
thesis.degree.department Aerospace Engineering and Engineering Mechanics
thesis.degree.discipline Aerospace Engineering
thesis.degree.grantor The University of Texas at Austin
thesis.degree.level Doctoral
thesis.degree.name Doctor of Philosophy

Files in this work

Download File: griesemerp60606.pdf
Size: 1.012Mb
Format: application/pdf

This work appears in the following Collection(s)

Show simple record


Advanced Search

Browse

My Account

Statistics

Information