Hardware and software were developed for the data evaluation of a flight measurement system consisting of inertial sensors on board the aircraft and ground-based flight path measurement stations. The results obtained are reference data for flight path, velocity, attitude angles and gyro drift. External measurements such as radar, cinetheodolites or TACAN, together with inertial data recorded in the aircraft, are evaluated by optimum smoothing techniques. Flight test results are presented.
Flight Testing of Inertial Navigation Systems: Hardware and Software Description
1983
93 pages
Report
Keine Angabe
Englisch
Inertial Navigation Systems Testing Handbooks
NTIS | 1976
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Tema Archiv | 1977
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AIAA | 1999
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NTRS | 1977
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