Files in this item



application/pdf9236436.pdf (7MB)Restricted to U of Illinois
(no description provided)PDF


Title:Optimal cooperative power-limited rendezvous
Author(s):Coverstone-Carroll, Victoria Lynn
Doctoral Committee Chair(s):Prussing, John E.
Department / Program:Aerospace Engineering
Discipline:Aerospace Engineering
Degree Granting Institution:University of Illinois at Urbana-Champaign
Subject(s):Engineering, Aerospace
Abstract:Minimum-fuel rendezvous of two power-limited low-thrust spacecraft is investigated. Both vehicles are active and provide thrust to complete the rendezvous. Total propellant consumption is minimized. Two gravitational field models are investigated: the Clohessy-Wiltshire linearized field and the inverse-square field. Analytical solutions are obtained for the linearized gravity field. A direct method using direct collocation with nonlinear programming is used for the nonlinear problem. Solutions obtained are checked against the primer vector necessary conditions for optimality. The optimal solutions depend in a complicated way on the power-to-mass ratios of the two spacecraft, the initial conditions, and the specified transfer time. Propellant and terminal orbit constraints are also discussed.
Issue Date:1992
Rights Information:Copyright 1992 Coverstone-Carroll, Victoria Lynn
Date Available in IDEALS:2011-05-07
Identifier in Online Catalog:AAI9236436
OCLC Identifier:(UMI)AAI9236436

This item appears in the following Collection(s)

Item Statistics