Inertial navigation system algorithmic correction methods were studied. Navigation system errors model calculation was carried out on board the aircraft. When calculating the models, it was proposed to ensure prefiltering of the measurement signals using a modified trend.
Signals prefiltering in the aircraft navigation system
XLIII ACADEMIC SPACE CONFERENCE: dedicated to the memory of academician S.P. Korolev and other outstanding Russian scientists – Pioneers of space exploration ; 2019 ; Moscow, Russia
AIP Conference Proceedings ; 2171 , 1
15.11.2019
4 pages
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
150006 Signals prefiltering in the aircraft navigation system
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