Simulink simulation of proportional navigation and command to line of sight missile guidance

Proportional Navigation and Command To Line Of Sight missile guidance are explored. A system flow graph is developed for each guidance technique. The block transfer functions are developed and a state space representation of the system is defined. The missile systems are then tested using one two-di...

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Main Author: Costello, Patrick.
Other Authors: Titus
Language:en_US
Published: Monterey, California. Naval Postgraduate School 2013
Online Access:http://hdl.handle.net/10945/31532
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spelling ndltd-nps.edu-oai-calhoun.nps.edu-10945-315322014-11-27T16:18:04Z Simulink simulation of proportional navigation and command to line of sight missile guidance Costello, Patrick. Titus Howard A Electrical Engineering Proportional Navigation and Command To Line Of Sight missile guidance are explored. A system flow graph is developed for each guidance technique. The block transfer functions are developed and a state space representation of the system is defined. The missile systems are then tested using one two-dimensional engagement and two three-dimensional engagement scenarios. The final three- dimensional scenario introduces measurement noise in order to evaluate the effect of noise on the guidance algorithms. The engagement results are then compared to analyze the miss distance of each type of missile guidance. 2013-04-29T22:51:20Z 2013-04-29T22:51:20Z 1995-03 Thesis http://hdl.handle.net/10945/31532 en_US This publication is a work of the U.S. Government as defined in Title 17, United States Code, Section 101. As such, it is in the public domain, and under the provisions of Title 17, United States Code, Section 105, it may not be copyrighted. Monterey, California. Naval Postgraduate School
collection NDLTD
language en_US
sources NDLTD
description Proportional Navigation and Command To Line Of Sight missile guidance are explored. A system flow graph is developed for each guidance technique. The block transfer functions are developed and a state space representation of the system is defined. The missile systems are then tested using one two-dimensional engagement and two three-dimensional engagement scenarios. The final three- dimensional scenario introduces measurement noise in order to evaluate the effect of noise on the guidance algorithms. The engagement results are then compared to analyze the miss distance of each type of missile guidance.
author2 Titus
author_facet Titus
Costello, Patrick.
author Costello, Patrick.
spellingShingle Costello, Patrick.
Simulink simulation of proportional navigation and command to line of sight missile guidance
author_sort Costello, Patrick.
title Simulink simulation of proportional navigation and command to line of sight missile guidance
title_short Simulink simulation of proportional navigation and command to line of sight missile guidance
title_full Simulink simulation of proportional navigation and command to line of sight missile guidance
title_fullStr Simulink simulation of proportional navigation and command to line of sight missile guidance
title_full_unstemmed Simulink simulation of proportional navigation and command to line of sight missile guidance
title_sort simulink simulation of proportional navigation and command to line of sight missile guidance
publisher Monterey, California. Naval Postgraduate School
publishDate 2013
url http://hdl.handle.net/10945/31532
work_keys_str_mv AT costellopatrick simulinksimulationofproportionalnavigationandcommandtolineofsightmissileguidance
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