Referenced Items are not available for this document.
Analytic expressions of the random errors in a satellite Doppler navigation system are developed. The errors in the along-track and across-track coordinates are expressed as functions of the geometry (range and angle), pass-length, and signal-to-noise ratio (SNR). Such an analytic result becomes possible due to an explicit solution to a simplified rectilinear model of the satellite pass over a flat Earth. It is shown that the explicit solution performance in the presence of noise is identical to that of the iterative solution, used in the real navigation problem.
Published in:
Aerospace and Electronic Systems, IEEE Transactions on
(Volume:AES-20
,
Issue:
6
)
Date of Publication: Nov. 1984
- Page(s):
- 810 - 816
- ISSN :
- 0018-9251
- Digital Object Identifier :
- 10.1109/TAES.1984.310464
- Product Type:
- Journals & Magazines
- Date of Current Version :
- 20 February 2007
- Issue Date :
- Nov. 1984
- Sponsored by :
- Aerospace & Electronic Systems Society
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.
