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Method and apparatus for contour mapping using synthetic aperture radarBy using two SAR antennas spaced a known distance, B, and oriented at substantially the same look angle to illuminate the same target area, pixel data from the two antennas may be compared in phase to determine a difference delta phi from which a slant angle theta is determined for each pixel point from an equation Delta phi = (2 pi B/lambda)sin(theta - alpha), where lambda is the radar wavelength and alpha is the roll angle of the aircraft. The height, h, of each pixel point from the aircraft is determined from the equation h = R cos theta, and from the known altitude, a, of the aircraft above sea level, the altitude (elevation), a', of each point is determined from the difference a - h. This elevation data may be displayed with the SAR image by, for example, quantizing the elevation at increments of 100 feet starting at sea level, and color coding pixels of the same quantized elevation. The distance, d, of each pixel from the ground track of the aircraft used for the display may be determined more accurately from the equation d = R sin theta.
Document ID
19860010240
Acquisition Source
Legacy CDMS
Document Type
Other - Patent
Authors
Goldstein, R. M.
(JPL Pasadena, Calif., United States)
Caro, E. R.
(JPL Pasadena, Calif., United States)
Wu, C.
(JPL Pasadena, Calif., United States)
Date Acquired
August 12, 2013
Publication Date
January 5, 1985
Subject Category
Earth Resources And Remote Sensing
Report/Patent Number
Patent Number: US-PATENT-4,551,724
Patent Application Number: US-PATENT-APPL-SN-465365
Patent Number: NASA-CASE-NPO-15939-1
Accession Number
86N19711
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-PATENT-4,551,724|NASA-CASE-NPO-15939-1
Patent Application
US-PATENT-APPL-SN-465365
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