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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Monterey, California. Naval Postgraduate School
2013
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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 |
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en_US |
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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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1716725220417470464 |