A Kalman filter application to the advanced tactical inertial guidance system of the air-launched low volume ramjet cruise missile.

A Montecarlo simulation is conducted to ascertain performance of the ATIGS system in a proposed air-launched cruise missile configuration. The simulation is conducted within a local-level inertial frame consisting of down-range, cross-range and up as primary reference vectors. Efforts are made to me...

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Bibliographic Details
Main Author: Van Devender, John Archite
Other Authors: NA
Language:en_US
Published: Monterey, California. Naval Postgraduate School 2012
Online Access:http://hdl.handle.net/10945/17829