Close category search window
 

DTEMS interferometric SAR design and method of baseline tilt determination

Sign In

Cookies must be enabled to login.After enabling cookies , please use refresh or reload or ctrl+f5 on the browser for the login options.

Formats Non-Member Member
$31 $13
Learn how you can qualify for the best price for this item!
Become an IEEE Member or Subscribe to
IEEE Xplore for exclusive pricing!
close button

puzzle piece

IEEE membership options for an individual and IEEE Xplore subscriptions for an organization offer the most affordable access to essential journal articles, conference papers, standards, eBooks, and eLearning courses.

Learn more about:

IEEE membership

IEEE Xplore subscriptions

1 Author(s)
Malliot, H.A. ; Res. & Dev. Div., Lockheed Martin Missiles & Space, Palo Alto, CA, USA

The Digital Terrain Elevation Mapping System (DTEMS) is a Lockheed Martin Missiles and Space (LMMS) commercial system for collection processing and archive of digital terrain matrix (DTM) and geometrically corrected ortho-rectified digital polarimetric radar imagery. DTEMS uses an ER-2 aircraft with an interferometric synthetic aperture radar (IFSAR) and differential GPS to develop a DTM in WGS84 rectangular coordinates with three meter post intervals. This paper describes the DTEMS X-band IFSAR design and presents the results of a system simulation which predicts that, for 45 degree or less terrain slope, DTEMS will achieve an average one σ relative elevation precision of 0.3 meter and absolute one σ elevation precision of 0.6 meter. The ER-2/IFSAR combination can provide up to 190,000 km2 of single flight area coverage. With this coverage DTEMS will be able to map the state of California in two flights and the entire United States, including Alaska, in 49 flights. SAR interferometer geometric baseline (IGB) tilt error is the major contributor to terrain elevation error. GPS interferometry (GPSI) and recursive IGB tilt estimation is used to reduce the IGB tilt knowledge error to less than 0.001 degree. The DTEMS implementation of GPSI uses GPS antennas installed on the top of each wing pod at positions just above the radar receiver antennas. In these positions the antennas have rigid coupling to the radar antennas and the 8.5 meter GPS IGB is close and parallel to the 8.5 m SAR IGB between the radar antenna phase centers. Consequently measurement of the GPS IGB attitude constitutes indirect measurement of the SAR IGB attitude

Published in:
Aerospace Applications Conference, 1996. Proceedings., 1996 IEEE  (Volume:4 )

Date of Conference: 3-10 Feb 1996

Need Help?


IEEE Advancing Technology for Humanity 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.