Nonlinear trajectory optimization with path constraints applied to spacecraft reconfiguration maneuvers

Nonlinear trajectory optimization with path constraints applied to spacecraft reconfiguration maneuvers

Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2005. === Includes bibliographical references (p. 115-120). === Future space assembly and science missions (e.g., Terrestrial Planet Finder) will typically require complex reconfiguration maneuvers involving...

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Bibliographic Details
Main Author: García, Ian Miguel
Other Authors: Jonathan P. How.
Format: Others
Language:English
Published: Massachusetts Institute of Technology 2006
Subjects:
Aeronautics and Astronautics.
Online Access:http://hdl.handle.net/1721.1/32448

Internet

http://hdl.handle.net/1721.1/32448

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