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

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
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spelling ndltd-nps.edu-oai-calhoun.nps.edu-10945-178292014-11-27T16:12:22Z A Kalman filter application to the advanced tactical inertial guidance system of the air-launched low volume ramjet cruise missile. Van Devender, John Archite NA NA NA 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 measure the relative effects associated with the intended pure position reset provided by a MICRAD sensor as compared with those effects which could be expected from a linear suboptimal Kalman filtering scheme used in conjuction with the MICRAD sensor 2012-11-16T18:48:03Z 2012-11-16T18:48:03Z 1976 Thesis http://hdl.handle.net/10945/17829 ocn640220765 en_US Monterey, California. Naval Postgraduate School
collection NDLTD
language en_US
sources NDLTD
description 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 measure the relative effects associated with the intended pure position reset provided by a MICRAD sensor as compared with those effects which could be expected from a linear suboptimal Kalman filtering scheme used in conjuction with the MICRAD sensor
author2 NA
author_facet NA
Van Devender, John Archite
author Van Devender, John Archite
spellingShingle Van Devender, John Archite
A Kalman filter application to the advanced tactical inertial guidance system of the air-launched low volume ramjet cruise missile.
author_sort Van Devender, John Archite
title A Kalman filter application to the advanced tactical inertial guidance system of the air-launched low volume ramjet cruise missile.
title_short A Kalman filter application to the advanced tactical inertial guidance system of the air-launched low volume ramjet cruise missile.
title_full A Kalman filter application to the advanced tactical inertial guidance system of the air-launched low volume ramjet cruise missile.
title_fullStr A Kalman filter application to the advanced tactical inertial guidance system of the air-launched low volume ramjet cruise missile.
title_full_unstemmed A Kalman filter application to the advanced tactical inertial guidance system of the air-launched low volume ramjet cruise missile.
title_sort kalman filter application to the advanced tactical inertial guidance system of the air-launched low volume ramjet cruise missile.
publisher Monterey, California. Naval Postgraduate School
publishDate 2012
url http://hdl.handle.net/10945/17829
work_keys_str_mv AT vandevenderjohnarchite akalmanfilterapplicationtotheadvancedtacticalinertialguidancesystemoftheairlaunchedlowvolumeramjetcruisemissile
AT vandevenderjohnarchite kalmanfilterapplicationtotheadvancedtacticalinertialguidancesystemoftheairlaunchedlowvolumeramjetcruisemissile
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