Referenced Items are not available for this document.
A fast 3-part method is introduced for the solution of the attitude of a low Earth orbit satellite using the GPS system as a source of phase information. A possibly novel method is used to overcome the well known integer ambiguity problem, involving the Gram Schmidt orthogonalization procedure at one stage and a fast replacement for the usual QUEST solution of the least mean square attitude solution
Published in:
Position Location and Navigation Symposium, IEEE 2000
Date of Conference: 2000
- Page(s):
- 132 - 139
- Meeting Date :
- 13 Mar 2000-16 Mar 2000
- Print ISBN:
- 0-7803-5872-4
- INSPEC Accession Number:
- 6656652
- Conference Location :
- San Diego, CA
- Digital Object Identifier :
- 10.1109/PLANS.2000.838294
- Product Type:
- Conference Publications
About IEEE Xplore | Contact | Help | Terms of Use | Nondiscrimination Policy | Site Map | Privacy & Opting Out of Cookies
A not-for-profit organization, IEEE is the world's largest professional association for the advancement of technology.
© Copyright 2013 IEEE - All rights reserved. Use of this web site signifies your agreement to the terms and conditions.
