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High dynamic GPS receiver validation demonstrationThe Validation Demonstration establishes that the high dynamic Global Positioning System (GPS) receiver concept developed at JPL meets the dynamic tracking requirements for range instrumentation of missiles and drones. It was demonstrated that the receiver can track the pseudorange and pseudorange rate of vehicles with acceleration in excess of 100 g and jerk in excess of 100 g/s, dynamics ten times more severe than specified for conventional High Dynamic GPS receivers. These results and analytic extensions to a complete system configuration establish that all range instrumentation requirements can be met. The receiver can be implemented in the 100 cu in volume required by all missiles and drones, and is ideally suited for transdigitizer or translator applications.
Document ID
19860009835
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Hurd, W. J.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Statman, J. I.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Vilnrotter, V. A.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
September 5, 2013
Publication Date
October 31, 1985
Subject Category
Aircraft Communications And Navigation
Report/Patent Number
NAS 1.26:176530
NASA-CR-176530
JPL-PUB-85-74
Report Number: NAS 1.26:176530
Report Number: NASA-CR-176530
Report Number: JPL-PUB-85-74
Accession Number
86N19306
Funding Number(s)
PROJECT: RTOP 644-11-00-03-20
CONTRACT_GRANT: NAS7-918
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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