On-orbit satellite inspection : navigation and [Delta]v analysis

Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2004. === In title on t.p., "[Delta]" appears as the upper-case Greek letter. === Includes bibliographical references (p. 213-215). === Since the late 1950's when the first man-made satellite...

Full description

Bibliographic Details
Main Author: Woffinden, David C., 1976-
Other Authors: David K. Geller and David Miller.
Format: Others
Language:en_US
Published: Massachusetts Institute of Technology 2005
Subjects:
Online Access:http://hdl.handle.net/1721.1/28862
id ndltd-MIT-oai-dspace.mit.edu-1721.1-28862
record_format oai_dc
spelling ndltd-MIT-oai-dspace.mit.edu-1721.1-288622019-05-02T16:29:51Z On-orbit satellite inspection : navigation and [Delta]v analysis Woffinden, David C., 1976- David K. Geller and David Miller. Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics. Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics. Aeronautics and Astronautics. Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2004. In title on t.p., "[Delta]" appears as the upper-case Greek letter. Includes bibliographical references (p. 213-215). Since the late 1950's when the first man-made satellite was launched into space, there has been a keen interest to inspect these orbiting spacecraft. In the past, there have been employed a variety of inspection methods which primarily consisted of different ground observation facilities. Unfortunately, ground-based sensors are often limited to the weather conditions and the particular flight path of the satellite. To overcome these and other obstacles, the inspection sensors can be moved from the ground and placed on spacecraft in orbit dedicated for satellite inspections. Is it possible for a miniaturized satellite to perform these inspections while on orbit? In this thesis, a small inspection satellite concept is developed and then verified using a high-fidelity 6 degree-of-freedom simulation. A detailed angles-only navigation analysis and [delta]v performance analysis of three different inspection trajectories are performed. The results of this analysis show the feasibility of angles-only rendezvous navigation and the over-all inspection satellite concept while validating the implemented flight algorithms. by David C. Woffinden. S.M. 2005-09-27T18:45:05Z 2005-09-27T18:45:05Z 2004 2004 Thesis http://hdl.handle.net/1721.1/28862 60410336 en_US M.I.T. theses are protected by copyright. They may be viewed from this source for any purpose, but reproduction or distribution in any format is prohibited without written permission. See provided URL for inquiries about permission. http://dspace.mit.edu/handle/1721.1/7582 215 p. 9556842 bytes 9584546 bytes application/pdf application/pdf application/pdf Massachusetts Institute of Technology
collection NDLTD
language en_US
format Others
sources NDLTD
topic Aeronautics and Astronautics.
spellingShingle Aeronautics and Astronautics.
Woffinden, David C., 1976-
On-orbit satellite inspection : navigation and [Delta]v analysis
description Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2004. === In title on t.p., "[Delta]" appears as the upper-case Greek letter. === Includes bibliographical references (p. 213-215). === Since the late 1950's when the first man-made satellite was launched into space, there has been a keen interest to inspect these orbiting spacecraft. In the past, there have been employed a variety of inspection methods which primarily consisted of different ground observation facilities. Unfortunately, ground-based sensors are often limited to the weather conditions and the particular flight path of the satellite. To overcome these and other obstacles, the inspection sensors can be moved from the ground and placed on spacecraft in orbit dedicated for satellite inspections. Is it possible for a miniaturized satellite to perform these inspections while on orbit? In this thesis, a small inspection satellite concept is developed and then verified using a high-fidelity 6 degree-of-freedom simulation. A detailed angles-only navigation analysis and [delta]v performance analysis of three different inspection trajectories are performed. The results of this analysis show the feasibility of angles-only rendezvous navigation and the over-all inspection satellite concept while validating the implemented flight algorithms. === by David C. Woffinden. === S.M.
author2 David K. Geller and David Miller.
author_facet David K. Geller and David Miller.
Woffinden, David C., 1976-
author Woffinden, David C., 1976-
author_sort Woffinden, David C., 1976-
title On-orbit satellite inspection : navigation and [Delta]v analysis
title_short On-orbit satellite inspection : navigation and [Delta]v analysis
title_full On-orbit satellite inspection : navigation and [Delta]v analysis
title_fullStr On-orbit satellite inspection : navigation and [Delta]v analysis
title_full_unstemmed On-orbit satellite inspection : navigation and [Delta]v analysis
title_sort on-orbit satellite inspection : navigation and [delta]v analysis
publisher Massachusetts Institute of Technology
publishDate 2005
url http://hdl.handle.net/1721.1/28862
work_keys_str_mv AT woffindendavidc1976 onorbitsatelliteinspectionnavigationanddeltavanalysis
_version_ 1719041793960443904