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Low cost tracking Navaids error model verificationFeatures and characteristics of the tracking navaids (Microwave Scanning Beam Landing System, Radar Altimeter, Tacan, rendezvous radar and one way Doppler extracter) were investigated. From the investigation, a set of specifications were developed for building equipment to verify the error model of the tracking navaids. Breadboard verification equipment (BVE) was built for the Microwave Scanning Beam Landing System and the radar altimeter. The breadboard verification equipment generates signals to the tracking navaids which simulate the space shuttles trajectory in the terminal area. The BVE simulates sources of navaids error by generating pseudorandom perturbations on the navaids signals. Differences between the trajectory value and the navaid derived values are taped and form the basis for the navaids error model.
Document ID
19750023123
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Charych, A.
(Airborne Instruments Lab. Deer Park, NY, United States)
Tatz, A.
(Airborne Instruments Lab. Deer Park, NY, United States)
Lovell, J.
(Airborne Instruments Lab. Deer Park, NY, United States)
Frederick, R.
(Airborne Instruments Lab. Deer Park, NY, United States)
Date Acquired
September 3, 2013
Publication Date
May 1, 1975
Subject Category
Space Communications, Spacecraft Communications, Command And Tracking
Report/Patent Number
NASA-CR-144443
Report Number: NASA-CR-144443
Accession Number
75N31196
Funding Number(s)
CONTRACT_GRANT: NAS9-14151
PROJECT: AIL PROJ. CO11-1
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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