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Measurement results from a balloon experiment simulating land mobile satellite transmissionsA transmitter operating at 869.525 MHz was twice carried by a stratospheric balloon to an altitude of about 40 km. A motor vehicle was driven within the line-of-sight from the transmitter. Measurements of the received signal strength were made every 1/8 wavelength for an overall travelling distance of about seven hundred kilometers. This scenario was to simulate a satellite system providing mobile communications to rural areas. The statistics of the sampled field, consisting of a combination of direct wave, specular reflection and diffuse components, are presented as a function of elevation angle. Parameters such as type of road driven (mostly 2 lane) or type of landscape (rolling to flat) and vegetation (pine and mixed forest) encountered are described where possible. The power distribution function for all the data, at elevation angles from 10 to 35 degrees, is 1 dB below the free space mean at the 50% level, 7 dB below at the 90% level, and 18 dB below at the 99% level. In the elevation angle range of 30 to 35 degrees the corresponding values were found to be .5, 1.2, and 4.5 dB. The conditional fade duration and level crossing rate distribution functions are also presented. The former shows some dependence on the threshold level, the latter almost none.
Document ID
19850017372
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Vogel, W. J.
(Texas Univ. Austin, TX, United States)
Torrence, G. W.
(Texas Univ. Austin, TX, United States)
Date Acquired
September 5, 2013
Publication Date
April 1, 1984
Subject Category
Communications And Radar
Report/Patent Number
JPL-9950-1049
NASA-CR-175740
NAS 1.26:175740
Report Number: JPL-9950-1049
Report Number: NASA-CR-175740
Report Number: NAS 1.26:175740
Accession Number
85N25683
Funding Number(s)
CONTRACT_GRANT: JPL-956520
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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