Efficient Trajectory Optimization Procedure for Designing Solar -Electric Propulsion, Gravity -Assist Outer -Planet Missions
Woo, Byoungsam
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https://hdl.handle.net/2142/85092
Description
Title
Efficient Trajectory Optimization Procedure for Designing Solar -Electric Propulsion, Gravity -Assist Outer -Planet Missions
Author(s)
Woo, Byoungsam
Issue Date
2004
Doctoral Committee Chair(s)
Coverstone, Victoria L.
Department of Study
Aerospace Engineering
Discipline
Aerospace Engineering
Degree Granting Institution
University of Illinois at Urbana-Champaign
Degree Name
Ph.D.
Degree Level
Dissertation
Date of Ingest
2015-09-25T22:34:24Z
Keyword(s)
Engineering, Aerospace
Language
eng
Abstract
A performance (delivered mass versus time of flight) estimation technique approximates the performance of different revolution ratio trajectories from a set of optimal trajectories using a linear least square fitting method. This technique brings further understanding of the effect of different revolution ratio outer-planet missions. It also provides performance prediction capability prior to generating optimal mission profiles.
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