NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Tests Of A Differential Global Positioning SystemPaper describes validation tests of global positioning system (GPS) for low-flying helicopters. Configured as differential GPS, in which components in both aircraft and ground station compute position errors relative to known location using satellite navigational data. Corrections computed from differences between computed and measured ranges to four satellites being tracked by receiver in both aircraft and ground systems. Tests conducted to determine whether equipment and computer programs of system operated correctly and consistently.
Document ID
19900000521
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Edwards, F. G.
(NASA Ames Research Center, Moffett Field, CA.)
Hegary, D. M.
(NASA Ames Research Center, Moffett Field, CA.)
Turner, R. N.
(Ohio Univ.)
Van Graas, F.
(Ohio Univ.)
Sharma, S.
(Ohio Univ.)
Date Acquired
August 14, 2013
Publication Date
October 1, 1990
Publication Information
Publication: NASA Tech Briefs
Volume: 14
Issue: 10
ISSN: 0145-319X
Subject Category
Electronic Systems
Report/Patent Number
ARC-12313
Accession Number
90B10521
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Available Downloads

There are no available downloads for this record.
No Preview Available