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University of Illinois at Urbana-Champaign
Efficient Trajectory Optimization Procedure for Designing Solar -Electric Propulsion, Gravity -Assist Outer -Planet Missions
Abstract
dc:descriptionA 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.
Degree
thesis:*- Name thesis:degree_name
- Ph.D.
- Level thesis:degree_level
- Dissertation
- Discipline thesis:degree_discipline
- Aerospace Engineering
- Grantor
- University of Illinois at Urbana-Champaign
- Year dc:date
- 2015
Author and committee
dc:creator, dc:contributor.*- Author dc:creator
-
- Woo, Byoungsam
- Contributors dc:contributor
-
- Coverstone, Victoria L.
Subjects
dc:subject × 1Rights
- Language dc:language
- eng
Identifiers
dc:identifier.*- Identifier
- (MiAaPQ)AAI3160973
- OAI identifier oai:identifier
- oai:www.ideals.illinois.edu:2142/85092