Abstract High-precision measurement systems of modern aircraft are studied in this paper. A measurement system with correction in the structure of inertial navigation system is introduced for highprecision aircraft. In the correction algorithms, a linear error model of the navigation system is usually used. With the aim of increasing the accuracy of the navigation system, we propose a nonlinear correction algorithm based on the state dependent coefficient representation of the nonlinear model.
Research on High-Precision Measurement Systems of Modern Aircraft
Russian Aeronautics ; 61 , 2 ; 279-286
2018-04-01
8 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
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