Instruments and data evaluation used in flight testing of the modular strapdown system (MSS) are described. Reference data, based on an inertial navigation system and optimal smoothing techniques, are shown for a flight test on the HFB 320 aircraft. The MSS flight tests were limited to the navigation part. The results show position errors of 10 km/hr maximum, speed errors of 8 m/sec maximum, elevation angle errors 0.4, and course error drift of 0.4/hr.
Flight Testing of a Strapdown System. Results of a Special Flight Test
1982
44 pages
Report
No indication
English
Flight test results of an integrated GPS and strapdown inertial system
Tema Archive | 1986
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