A strapdown system is considered as an unaided inertial navigator aboard an aircraft. Presented here are simulation results detailing the propagation of navigation errors. Several of the error mechanisms are discussed at length and a set of linearized differential equations which can be used to analyze error propagation is presented.
Propagation and system accuracy impact of major sensor errors on a strapdown aircraft navigator
Fortpflanzung und Systemgenauigkeitsaufschlag der groesseren Messfehler eines nicht kardanisch befestigten Flugzeugnavigators
IEEE Transactions on Aerospace and Electronic Systems ; 9 , 6 ; 838-846
1973
9 Seiten, 11 Bilder, 1 Tabelle, 7 Quellen
Article (Journal)
English