Accession Number : AD0705256
Title : A DOPPLER INERTIAL INVESTIGATION.
Descriptive Note : Technical rept.,
Corporate Author : ARMY ELECTRONICS COMMAND FORT MONMOUTH NJ
Personal Author(s) : Galanti, Carl J. ; Levine, Irving
Report Date : MAR 1970
Pagination or Media Count : 58
Abstract : An error analysis of a hybrid doppler-inertial system (second order) was performed with an without noise error sources. From this analysis it was determined that the doppler is the key contributor to the velocity error of the system. Also, a procedure for selecting the parameters of a doppler-inertial system for minimum cost and maximum performance was derived. (Author)
Descriptors : *DOPPLER NAVIGATION, *INERTIAL NAVIGATION, HELICOPTERS, INSTRUMENTATION, ERROR ANALYSIS, NOISE(RADIO).
Subject Categories : Air Navigation and Guidance
Distribution Statement : APPROVED FOR PUBLIC RELEASE