Skymark selection algorithm for a space-based navigational concept

Thesis (M. Eng.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2002.

Bibliographic Details
Main Author: Kaptuch, James A. (James Anthony), 1979-
Other Authors: Richard Phillips.
Format: Thesis
Language:en_US
Published: Massachusetts Institute of Technology 2005
Subjects:
Online Access:http://hdl.handle.net/1721.1/26898
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author Kaptuch, James A. (James Anthony), 1979-
author2 Richard Phillips.
author_facet Richard Phillips.
Kaptuch, James A. (James Anthony), 1979-
author_sort Kaptuch, James A. (James Anthony), 1979-
collection MIT
description Thesis (M. Eng.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2002.
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spelling mit-1721.1/268982019-04-12T11:13:43Z Skymark selection algorithm for a space-based navigational concept Kaptuch, James A. (James Anthony), 1979- Richard Phillips. Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics. Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics. Aeronautics and Astronautics. Thesis (M. Eng.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2002. Includes bibliographical references (p. 161). The angles-only navigational concept envisions using orbiting satellites and other space objects as a set of moving landmarks, or skymarks, to improve upon an observer's knowledge of its position in space. This is accomplished by taking line of sight, or angles-only, measurements from an observer to a skymark using a modified star tracker, and then making use of triangulation to estimate the observer's location. A Kalman filter is used to update the observer's knowledge of its state, and the uncertainty concomitant with that knowledge can then be determined. This thesis covers the development of an algorithm for selecting four successive skymarks to be viewed by an observer, with a goal of minimizing both the observer's error in its position estimate and the time required to make the selection. During the development process a number of different algorithms were developed and compared, both with one another and with an algorithm that determined the optimal answer, in order to determine the one that best met the above criteria. Factors taken into account by the various algorithms include the geometry of the four observed skymarks, the distance between observer and skymark, the errors associated with the observer's knowledge of the skymark's state, and the effects of the observer's motion on error propagation. by James A. Kaptuch. M.Eng. 2005-09-06T20:43:14Z 2005-09-06T20:43:14Z 2002 2002 Thesis http://hdl.handle.net/1721.1/26898 54090452 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 161 p. 12644223 bytes 12665719 bytes application/pdf application/pdf application/pdf Massachusetts Institute of Technology
spellingShingle Aeronautics and Astronautics.
Kaptuch, James A. (James Anthony), 1979-
Skymark selection algorithm for a space-based navigational concept
title Skymark selection algorithm for a space-based navigational concept
title_full Skymark selection algorithm for a space-based navigational concept
title_fullStr Skymark selection algorithm for a space-based navigational concept
title_full_unstemmed Skymark selection algorithm for a space-based navigational concept
title_short Skymark selection algorithm for a space-based navigational concept
title_sort skymark selection algorithm for a space based navigational concept
topic Aeronautics and Astronautics.
url http://hdl.handle.net/1721.1/26898
work_keys_str_mv AT kaptuchjamesajamesanthony1979 skymarkselectionalgorithmforaspacebasednavigationalconcept