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Multipath analysis diffraction calculationsThis report describes extensions of the Kirchhoff diffraction equation to higher edge terms and discusses their suitability to model diffraction multipath effects of a small satellite structure. When receiving signals, at a satellite, from the Global Positioning System (GPS), reflected signals from the satellite structure result in multipath errors in the determination of the satellite position. Multipath error can be caused by diffraction of the reflected signals and a method of calculating this diffraction is required when using a facet model of the satellite. Several aspects of the Kirchhoff equation are discussed and numerical examples, in the near and far fields, are shown. The vector form of the extended Kirchhoff equation, by adding the Larmor-Tedone and Kottler edge terms, is given as a mathematical model in an appendix. The Kirchhoff equation was investigated as being easily implemented and of good accuracy in the basic form, especially in phase determination. The basic Kirchhoff can be extended for higher accuracy if desired. A brief discussion of the method of moments and the geometric theory of diffraction is included, but seems to offer no clear advantage in implementation over the Kirchhoff for facet models.
Document ID
19960042553
Acquisition Source
Langley Research Center
Document Type
Contractor Report (CR)
Authors
Statham, Richard B.
(Lockheed Martin Engineering and Sciences Co. Hampton, VA United States)
Date Acquired
September 6, 2013
Publication Date
May 1, 1996
Subject Category
Spacecraft Instrumentation
Report/Patent Number
LPO-SASS-96-1
NAS 1.26:198314
NASA-CR-198314
Report Number: LPO-SASS-96-1
Report Number: NAS 1.26:198314
Report Number: NASA-CR-198314
Accession Number
96N31529
Funding Number(s)
PROJECT: RTOP 478-87-00-01
CONTRACT_GRANT: NAS1-19000
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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