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