Multiple satellite trajectory optimization
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Authors
Mendy, Paul B., Jr.
Subjects
Satellite trajectory control
Multi-agent optimization
Optimal control
DIDO
Dynamic optimization
Multi-agent optimization
Optimal control
DIDO
Dynamic optimization
Advisors
Ross, I. Michael
Danielson, D.A.
Date of Issue
2004-12
Date
December 2004
Publisher
Monterey California. Naval Postgraduate School
Language
Abstract
problem, with engine thrust as the only possible perturbation. The optimal control problems are solved using the general purpose dynamic optimization software, DIDO. The dynamical model together with the fuel optimal control problem is validated by simulating several well known orbit transfers. By replicating the single satellite model, this thesis shows that a multi-satellite model which optimizes all vehicles concurrently can be easily built. The specific scenario under study involves the injection of multiple satellites from a common launch vehicle; however, the methods and model are applicable to spacecraft formation problems as well.
Type
Thesis
Description
Series/Report No
Department
Mechanical and Astronautical Engineering (MAE)
Organization
Naval Postgraduate School (U.S.)
Identifiers
NPS Report Number
Sponsors
Funder
Format
xiv, 95 p.: col. ill.
Citation
Distribution Statement
Approved for public release; distribution is unlimited.
Rights
This publication is a work of the U.S. Government as defined in Title 17, United States Code, Section 101. Copyright protection is not available for this work in the United States.