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Investigation of new techniques for aircraft navigation using the omega navigationAn OMEGA navigation receiver with a microprocessor as the computational component was investigated. A version of the INTEL 4004 microprocessor macroassembler suitable for use on the CDC-6600 system and development of a FORTRAN IV simulator program for the microprocessor was developed. Supporting studies included development and evaluation of navigation algorithms to generate relative position information from OMEGA VLF phase measurements. Simulation studies were used to evaluate assumptions made in developing a navigation equation in OMEGA Line of Position (LOP) coordinates. Included in the navigation algorithms was a procedure for calculating a position in latitude/longitude given an OMEGA LOP fix. Implementation of a digital phase locked loop (DPLL) was evaluated on the basic of phase response characteristics over a range of input phase variations. Included also is an analytical evaluation on the basis of error probability of an algorithm for automatic time synchronization of the receiver to the OMEGA broadcast format. The use of actual OMEGA phase data and published propagation prediction corrections to determine phase velocity estimates was discussed.
Document ID
19780009094
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Baxa, E. G., Jr.
(Research Triangle Inst. Research Triangle Park, NC, United States)
Date Acquired
September 3, 2013
Publication Date
February 1, 1978
Subject Category
Aircraft Communications And Navigation
Report/Patent Number
NASA-CR-145303
RTI-4378-1152-F
Report Number: NASA-CR-145303
Report Number: RTI-4378-1152-F
Accession Number
78N17037
Funding Number(s)
CONTRACT_GRANT: NAS1-14005
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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