Kill vehicle effectiveness for boost phase interception of ballistic missiles
Approved for public release; distribution is unlimited === Boost phase interception of ballistic missiles is envisioned as the primary response of the layered defense architecture implemented in the ballistic missile defense system. A limited time frame in which to take action and the necessity to i...
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ndltd-nps.edu-oai-calhoun.nps.edu-10945-16092017-05-24T16:07:12Z Kill vehicle effectiveness for boost phase interception of ballistic missiles Bardanis, Florios Pace, Phillip E. Tummala, Murali Naval Postgraduate School (U.S.). Electrical and Computer Engineering Ballistic missile defenses Electrical engineering Proportional navigation Intermediate-range ballistic missiles Approved for public release; distribution is unlimited Boost phase interception of ballistic missiles is envisioned as the primary response of the layered defense architecture implemented in the ballistic missile defense system. A limited time frame in which to take action and the necessity to implement hit-to-kill technology in the kill vehicle counterbalances the many advantages of boost phase interception. Direct hit missile technology is constrained by the requirement to minimize miss distance to a negligible amount between the kill vehicle and optimum aimpoint on the target. This thesis examines kill vehicle effectiveness, which is tantamount to miss distance, as a function of both the kill vehicle maximum acceleration capability and the guidance system time constant necessary to destroy a target. The kill vehicle guidance system is modeled in MATLAB as a fifth-order binomial series with proportional navigation. The simulation examines the effect of an accelerating target attributed to powered flight and aimpoint displacement caused by a shift in tracking point from the target plume to the payload when resolution occurs. The kill vehicle minimum requirements as indi-cated by the simulation include a lateral acceleration capability of four times the target acceleration and a guidance system time constant that is less than one-tenth the estimated flight time. Lieutenant, Canadian Navy 2012-03-14T17:32:26Z 2012-03-14T17:32:26Z 2004-06 Thesis http://hdl.handle.net/10945/1609 Copyright is reserved by the copyright owner. xvi, 51 p. : ill. (some col.) ; application/pdf Monterey, California. Naval Postgraduate School |
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Ballistic missile defenses Electrical engineering Proportional navigation Intermediate-range ballistic missiles |
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Ballistic missile defenses Electrical engineering Proportional navigation Intermediate-range ballistic missiles Bardanis, Florios Kill vehicle effectiveness for boost phase interception of ballistic missiles |
description |
Approved for public release; distribution is unlimited === Boost phase interception of ballistic missiles is envisioned as the primary response of the layered defense architecture implemented in the ballistic missile defense system. A limited time frame in which to take action and the necessity to implement hit-to-kill technology in the kill vehicle counterbalances the many advantages of boost phase interception. Direct hit missile technology is constrained by the requirement to minimize miss distance to a negligible amount between the kill vehicle and optimum aimpoint on the target. This thesis examines kill vehicle effectiveness, which is tantamount to miss distance, as a function of both the kill vehicle maximum acceleration capability and the guidance system time constant necessary to destroy a target. The kill vehicle guidance system is modeled in MATLAB as a fifth-order binomial series with proportional navigation. The simulation examines the effect of an accelerating target attributed to powered flight and aimpoint displacement caused by a shift in tracking point from the target plume to the payload when resolution occurs. The kill vehicle minimum requirements as indi-cated by the simulation include a lateral acceleration capability of four times the target acceleration and a guidance system time constant that is less than one-tenth the estimated flight time. === Lieutenant, Canadian Navy |
author2 |
Pace, Phillip E. |
author_facet |
Pace, Phillip E. Bardanis, Florios |
author |
Bardanis, Florios |
author_sort |
Bardanis, Florios |
title |
Kill vehicle effectiveness for boost phase interception of ballistic missiles |
title_short |
Kill vehicle effectiveness for boost phase interception of ballistic missiles |
title_full |
Kill vehicle effectiveness for boost phase interception of ballistic missiles |
title_fullStr |
Kill vehicle effectiveness for boost phase interception of ballistic missiles |
title_full_unstemmed |
Kill vehicle effectiveness for boost phase interception of ballistic missiles |
title_sort |
kill vehicle effectiveness for boost phase interception of ballistic missiles |
publisher |
Monterey, California. Naval Postgraduate School |
publishDate |
2012 |
url |
http://hdl.handle.net/10945/1609 |
work_keys_str_mv |
AT bardanisflorios killvehicleeffectivenessforboostphaseinterceptionofballisticmissiles |
_version_ |
1718452682524459008 |