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Dissertations / Theses on the topic 'Missile attacks'

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Published: 5 June 2025

Last updated: 16 July 2025

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1

Almeida, Rui. "Probability models for defense against missile attacks." Thesis, Monterey, California. Naval Postgraduate School, 1991. http://hdl.handle.net/10945/28466.

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2

Hogue, David W. "How integrating a shipboard radar system to a[n] electronic warfare system can help defeat anti-ship missile attacks." Master's thesis, This resource online, 1993. http://scholar.lib.vt.edu/theses/available/etd-03302010-020309/.

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3

Song, Shing-Jen. "Probability models for assessing the value of battle damage assessment in the defense against sequential theater missile attacks." Thesis, Monterey, Calif. : Springfield, Va. : Naval Postgraduate School ; Available from National Technical Information Service, 1996. http://handle.dtic.mil/100.2/ADA311138.

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Thesis (M.S. in Operations Research) Naval Postgraduate School, March 1996.<br>Thesis advisor(s): Donald P. Gaver, Patricia A. Jacobs. "March 1996." Includes bibliographical references. Also Available online.

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4

Demir, Ali. "Tomahawk land attack missile predesignation : optimization revisited /." Thesis, Monterey, Calif. : Springfield, Va. : Naval Postgraduate School ; Available from National Technical Information Service, 2004. http://library.nps.navy.mil/uhtbin/hyperion/04Jun%5FDemir.pdf.

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5

Townsend, James R. "Defense of Naval Task Forces from Anti-Ship Missile attack." Thesis, Monterey, Calif. : Springfield, Va. : Naval Postgraduate School ; Available from National Technical Information Service, 1999. http://handle.dtic.mil/100.2/ADA363038.

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6

Haberlin, Richard J. "Analysis of unattended ground sensors in theater Missile Defense Attack Operations." Thesis, Monterey, California. Naval Postgraduate School, 1997. http://hdl.handle.net/10945/26369.

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Approved for public release; distribution is unlimited<br>Unattended ground sensors have a tremendous potential for improving Tactical Ballistic Missile Attack Operations. To date, however, this potential has gone unrealized primarily due to a lack of confidence in the systems and a lack of tactical doctrine for their employment. This thesis provides analyses to demonstrate the effective use of sensor technology and provides recommendations as to how they may best be employed. The probabilistic decision model reports the optimal size array for each of the candidate array locations. It also pro

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7

Johnston, Michael S. "An analysis on the survivability of Land Attack Missiles (LAM)." Thesis, Monterey, Calif. : Springfield, Va. : Naval Postgraduate School ; Available from National Technical Information Service, 2000. http://handle.dtic.mil/100.2/ADA387374.

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Thesis (M.S. in Operations Research) Naval Postgraduate School, Dec. 2000.<br>"December 2000." Thesis advisor(s): Thomas W. Lucas. Includes bibliographical references (p. 91-92). Also available online.

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8

Pèrez, Juan-Pablo. "Analysis of the deceleration signal of a missile during a hard-target attack." Thesis, National Library of Canada = Bibliothèque nationale du Canada, 1997. http://www.collectionscanada.ca/obj/s4/f2/dsk2/ftp04/mq25701.pdf.

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9

Johnson, Dan A. "Flowfield measurements in the wake of a missile at high angle of attack." Thesis, Monterey, California. Naval Postgraduate School, 1989. http://hdl.handle.net/10945/27059.

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10

Cetiner, Abdullah Emre. "Split Canard Design For Enhancing The Maneuverability Of A Missile At High Angles Of Attack." Master's thesis, METU, 2012. http://etd.lib.metu.edu.tr/upload/12614920/index.pdf.

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In this thesis, the effects of split canard on the aerodynamic characteristics of missiles at high angles of attack are numerically investigated. Moreover, an enhanced semi-empirical engineering-level method is developed for prediction of normal force and pitching moment of split canard mounted missiles. In order to analyze the effects of split canard, a generic test case model is created by mounting a split canard to a generic test case model, NASA Dual Control Missile (NDCM), which was previously modeled and analyzed for the validation of CFD modeling. After obtaining a generic missile model

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11

Lanier, Cathy L. "Preventing terror attacks in the Homeland : a new mission for state and local police." Thesis, Monterey, Calif. : Springfield, Va. : Naval Postgraduate School ; Available from National Technical Information Service, 2005. http://library.nps.navy.mil/uhtbin/hyperion/05Sep%5FLanier.pdf.

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Thesis (M.A. in Security Studies (Homeland Security and Defense))--Naval Postgraduate School, September 2005.<br>Thesis Advisor(s): Christopher Bellavita. Includes bibliographical references (p.61-63). Also available online.

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12

Lung, Ming-Hung. "Flowfield measurements in the vortex wake of a missile at high angle of attack in turbulence." Thesis, Monterey, California. Naval Postgraduate School, 1988. http://hdl.handle.net/10945/23235.

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Approved for public release; distribution is unlimited<br>The flowfield downstream of a vertically-launched surface-to-air missile model at an angle of attack of 50° and a Reynolds number of 1.1 x 10(5) was investigated in a wind tunnel of the Naval Postgraduate School. The goal of this thesis is to experimentally validate the pressure measurement system for flowfield variables with elevated levels of turbulence; to determine the location and intensity of the asymmetric vortices in the wake of the VLSAM model at a raised level of freestream turbulence; and to display the asymmetric vortices by

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13

Reynolds, Guy B. "The nuclear-armed Tomahawk Cruise Missile : its potential utility on United States and United Kingdom attack submarines /." Thesis, Monterey, Calif. : Springfield, Va. : Naval Postgraduate School ; Available from National Technical Information Service, 1998. http://handle.dtic.mil/100.2/ADA359545.

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Thesis (M.A. in National Security Affairs) Naval Postgraduate School, December 1998.<br>"December 1998." Thesis advisor(s): David S. Yost, James J. Wirtz. Includes bibliographical references (p. 65-68). Also available online.

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14

Yildiz, Kursad. "Electronic attack and sensor fusion techniques for boot-phase defense against multiple ballistic threat missiles." Thesis, Monterey, Calif. : Springfield, Va. : Naval Postgraduate School ; Available from National Technical Information Service, 2005. http://library.nps.navy.mil/uhtbin/hyperion/05Jun%5FYildiz.pdf.

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Thesis (M.S. in Systems Engineering)--Naval Postgraduate School, June 2005.<br>Thesis Advisor(s): Phillip E. Pace, Murali Tummala. Includes bibliographical references (p.155-158). Also available online.

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15

Lotrionte, Catherine B. "The missing piece why intelligence reform failed after 9/11 /." Connect to Electronic Thesis (ProQuest), 2008. http://0-gateway.proquest.com.library.lausys.georgetown.edu/openurl?url_ver=Z39.88-2004&rft_val_fmt=info:ofi/fmt:kev:mtx:dissertation&res_dat=xri:pqdiss&rft_dat=xri:pqdiss:3315459.

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16

Dryer, David A. "An analysis of ground maneuver concentration during NTC deliberate attack missions and its influence on mission effectiveness." Thesis, Monterey, California. Naval Postgraduate School, 1989. http://hdl.handle.net/10945/26864.

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17

Tekin, Raziye. "Design, Modeling, Guidance And Control Of A Vertical Launch Surface To Air Missile." Master's thesis, METU, 2010. http://etd.lib.metu.edu.tr/upload/12612408/index.pdf.

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The recent interests in the necessity of high maneuverability and vertical launching triggered namely the unconventional control design techniques that are effective at high angle of attack flight regimes. For most of missile configurations, this interest required thrust vector control together with conventional aerodynamic control. In this study, nonlinear modeling and dynamical analysis of a surface to air missile with both aerodynamic and thrust vector control is investigated. Aerodynamic force and moment modeling of the presented missile includes the challenging high angle of attack aero

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18

Morris, Jason T. "Information management utilizing Valued Information at the Right Time (VIRT) as applied to a Joint Terminal Attack Controller (JTAC) mission." Thesis, Monterey, Calif. : Naval Postgraduate School, 2008. http://bosun.nps.edu/uhtbin/hyperion-image.exe/08Mar%5FMorris.pdf.

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Thesis (M.S. in Information Technology Management)--Naval Postgraduate School, March 2008.<br>Thesis Advisor(s): Hayes-Roth, Rick. "March 2008." Description based on title screen as viewed on May 5, 2008. Includes bibliographical references (p. 57-58). Also available in print.

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19

Lošťák, Miroslav. "Bezpečnost dopravního letounu při poškození draku teroristickým útokem." Doctoral thesis, Vysoké učení technické v Brně. Fakulta strojního inženýrství, 2012. http://www.nusl.cz/ntk/nusl-234007.

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Modern-day terrorist attacks present a considerable danger for commercial aircrafts. This thesis analyzes potential methods of such attacks with a critical analysis of the most dangerous type: an attack from the outside of the aircraft via a fragmentation missile warhead. Such missiles cause damage to the airframe of the aircraft through fragments created by the explosion. In this thesis, analytical geometry is used to determine the area of the aircraft affected by the fragmentation. The aircraft’s geometry and the fragments’ dispersion are calculated by analytical functions, and the effect of

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20

Li, Pu-Chao, and 李步超. "Runway Damage Assessment under Ballistic Missile Attack." Thesis, 2010. http://ndltd.ncl.edu.tw/handle/24659275849243796922.

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碩士<br>國防大學管理學院<br>資訊管理學系<br>99<br>Ballistic missile has excellent penetration capability because of its long-range and fast speed features. Therefore, if the conflict erupts in the Taiwan Strait, the PRC might use its ballistic missile force to attack targets in Taiwan of strategic and tactical importance, such as airport, in order to gain air superiority and initiate next waves of attack so as to occupy Taiwan Proper. Owing to the dynamic nature in the battlefield and the ever-evolving high-tech weapons with multifunctional capabilities, we, as the ROC nationals in Taiwan, are concerned about

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21

白鴻慶. "Robust Missile Control Under High Angle of Attack." Thesis, 2001. http://ndltd.ncl.edu.tw/handle/48794969159919819727.

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碩士<br>國立成功大學<br>航空太空工程學系<br>89<br>An autopilot system for the heading reversal maneuvering (HRM) phase in missile engagement with high off-boresight angle up to 180 degrees has been successfully synthesized with the combination of aerodynamic control and thrust vector control (TVC). The application of H∞ control theory has provided the missile robustness (including robust stability and robust performance) properties in the presence of model uncertainty caused by aerodynamic coefficient variation. Simultaneously, autopilot has enabled the missile to resist the maximal possible yawing moment wit

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22

Hsu, Li-Ling, and 許莉玲. "An analysis of ballistic missile attack on airbase." Thesis, 2010. http://ndltd.ncl.edu.tw/handle/27164245642666377149.

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23

Chen, Yi-Wen, and 陳怡文. "The Runway Blockading Operation Assessment under Tactical Ballistic Missile Attack." Thesis, 2009. http://ndltd.ncl.edu.tw/handle/73629808312771451410.

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碩士<br>國防大學管理學院<br>資源管理及決策研究所<br>97<br>There are many parameters and considerations concerning runway blockading operation. This study takes almost every variable into account, including attack/ defense strategy, blockading/ anti-blockading operations to build a simulation model. This model consists of a Markov ballistic missile defense model and uses Monte Carlo simulation to describe random phenomenon. The required parameters input include attacker’s strategy, weapon performance and defender’s strategy, emergency repair ability, runway size and minimum operating strip. The outputs of the mode

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24

Engelbrecht, Gerhard Nieuwoudt. "On optimising FAC(M) counter missile tactics : a dynamic simulation model to optimise soft kill tactics employed by a generic fast attack craft against a generic surface-to-surface, fire-and-forget missile." Diss., 1997. http://hdl.handle.net/10500/16747.

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The aim of this dissertation is to show how counter missile tactics for a fast attack craft armed with missiles [FAC(M)] against a surface-to-surface, fireand- forget missile [SSM] can be optimised. As a result the ship and missile will be modelled as generic concepts while the environment will be a chosen area of operations. The applicable methodology is to simulate the ship, missile and environment as well as the interactions between them. At the same time, the ship will be carrying out combinations of five separate missile counter measures. The methodology is then to build a dynamic

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25

Hwang, Jian-Hua, and 黃建華. "Numerical Simulation of Flow over a Missile at High Angle of Attack." Thesis, 2003. http://ndltd.ncl.edu.tw/handle/39524046461859908398.

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碩士<br>國立成功大學<br>航空太空工程學系碩博士班<br>91<br>A numerical method is developed to study the flow field over a missile at high angle of attack. The method solves the compressible Navier-Stokes equations. It uses a third-order upwind finite-volume scheme for discretizing the convective terms and a second-order central finite-volume scheme for discretizing the viscous terms. A DDADI time integration coupling with an implicit residual smoothing is used for achieving fast convergence. A Flow over a tangent ogive-forebody is tested to verify the numerical method. At same Reynolds number，the flows past a

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26

Chou, Hung-Shen, and 周宏聲. "Visualization of Transonic Flow over a Missile Body at High-Angle-of-Attack." Thesis, 2000. http://ndltd.ncl.edu.tw/handle/39940606958270826603.

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碩士<br>國立成功大學<br>航空太空工程學系<br>88<br>The purpose of this study is to investigate the aerodynamic characteristics of the ogive-cylinder by means of visualization at high angle of attack with lateral jet. Furthermore, the pressure sensitive paint (PSP) technique for measuring pressure distribution on aerodynamic surfaces was studied. This experiment includes three parts. (1) By means of a dye-injection method employed in a water channel and the flow region of the separated vortex sheets was studied. Applying the paint-dots method showed the limiting streamline and separation line pattern on the mod

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27

Rabang, M. Peter. "Turbulence effects on the high angle of attack aerodynamics of a vertically launched missile." Thesis, 1988. http://hdl.handle.net/10945/23433.

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28

Kistan, Prevani. "Numerical Investigation of Strakes and Strakelets on a Missile at High Angles of Attack." Thesis, 2007. http://hdl.handle.net/10539/2152.

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Student Number : 9803192Y - MSc(Eng) Dissertation - School of Mechanical, Industrial and Aeronautical Engineering - Faculty of Engineering and the Built Environment<br>A computational °uid dynamics (CFD) study was carried out to improve the aero- dynamic performance of an agile high angle of attack missile. The normal force generated by the missile strakes had to be increased at the low angles of attack and the large side forces, experienced at high angles of attack due to the formation of steady asymmetric vortices had to be eliminated using strakelets on the missile nose. The ¯rst ob

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29

曾瑞欽. "High Attack Angle Autopilot Design of a Bank-to-turn Missile with a Reaction Jet." Thesis, 2002. http://ndltd.ncl.edu.tw/handle/38574529490315625328.

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碩士<br>國立臺灣大學<br>電機工程學研究所<br>90<br>In this thesis, we’ll discuss how to combine the Bank-to-turn missile and Reaction jet system. In the research before, we know the Bank-to-turn missile have higher mobility than the Skid -to-turn missile, but we now face the ballistic missile, which have the relative advantage in velocity. Beside, It is lack of aerodynamics in the high air, it well loss the control ability of the Bank-to-turn missile. So how to integrate the Reaction jet system and the Bank-to-turn missile system to improve the manipulator ability become the main subject of this thesis.

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30

CHEN, YI-YEN, and 陳懿言. "Simplified Swarm Optimization for the Crafts Rostering Problem of Naval Missile Fast-Attack Craft Squadron." Thesis, 2018. http://ndltd.ncl.edu.tw/handle/c8x6k7.

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碩士<br>國防大學<br>資源管理及決策研究所<br>106<br>The Fast-attack craft combat squadron is one of the naval tactical units in R.O.C.. Every day, a certain number of crafts must be arranged into combat readiness for emergency situations. This study proposed a novel craft rostering problem (CRP) whose purpose is to schedule crafts to fulfil daily tasks according to a mission list under some constraints. In nature, the problem is a multi-objective problem which simultaneously minimizes the fairness of task assignment, the density of tasks, and the number of task-switching. First, to model by multi-objective opt

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31

Liu, Horng-Di, and 劉鴻第. "An Application of Monte Carlo Methods on Military Operations-Assessments of Ballistic Missile Attack on Airfields." Thesis, 2006. http://ndltd.ncl.edu.tw/handle/74692390695536428257.

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碩士<br>逢甲大學<br>工業工程與系統管理學研究所<br>94<br>Recently China has brought in vast international investment and commercial technology. With lower rate of human labor, China takes an advantage in commercial production and global marketing which makes main land China to create great economy growth. Definitely, huge amount of foreign exchange earnings provides firm support of their “military modernization”. Navy, Air power, and surface to surface missile are main infrastructure of their scheme. With long range, high speed, hard to be detected and intercepted, ballistic missiles are considered the most criti

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32

Roane, Donald P. Jr, and Richard M. Howard. "The effect of a turbulent airstream on a vertically-launched missile at high angles of attack." Thesis, 1987. http://hdl.handle.net/10945/22249.

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33

Chen, Chih-Chieh, and 陳智杰. "Experimental study of Wake Properties & Dynamic Force of Missile-Typed Circular Cylinder at High Angle of Attack." Thesis, 1993. http://ndltd.ncl.edu.tw/handle/83926134075839688212.

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34

Chio, Wen-Bin, and 邱文彬. "An Experimental Study on the Oil Film Method and Pressure of a Missile Body at High-angle-of Attack with Lateral Jet." Thesis, 2000. http://ndltd.ncl.edu.tw/handle/27477166748145994979.

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碩士<br>國立成功大學<br>航空太空工程學系<br>88<br>The purpose of the study is to investigate the tangent ogive forebody fineness ratio of 2 at high angle of attack tested in transonic regime. The Mach numbers performed in wind tunnel are 0.3, 0.6, 0.78 and 0.86, respectively, and the corresponding Reynolds numbers, based on the diameter of missile, are 、、 and , respectively. The angle of attacks chosen in the experiments are and , respectively. The experiments were conducted in a 600mm 600mm transonic wind tunnel located at the Aerospace Science and Technology Research Center of National Cheng-Kung Uni

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35

許鈺祥. "Exploring the Crisis Response Strategy and Reputation of R.O.C Military from the Cognitive Gap Perspective – A Case Study of the Fast Attack Craft Guided Missile." Thesis, 2018. http://ndltd.ncl.edu.tw/handle/grhe38.

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碩士<br>國防大學政治作戰學院<br>新聞碩士班<br>106<br>The R.O.C military must deal with "crisis" very carefully, to protect its image and reputation from the citizens. The very first principle of resolving the crisis is to carry out "crisis communication." The focus is on reducing the harm of the crisis to the organization so that the target audience can accept the organization's response to crisis events. On the night of March 18, 2017, the Navy's Fast Attack Craft Guided missile collided with an entertainment fishing boat. Although the Navy had explained to the public that weather factors caused the incident,

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36

Abdul, Saleem P. K. "Guidance Laws for Engagement Time Control." Thesis, 2016. http://etd.iisc.ac.in/handle/2005/2926.

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Autonomous aerial vehicles like missiles and unmanned aerial vehicles (UAVs) have attracted various military and civilian applications. The primary guidance objective of any autonomous vehicle is to reach the desired destination point (target or waypoint). However, many practical engagements impose additional constraints like minimum control effort, a desired final velocity direction or a predefined engagement time. This thesis addresses engagement time constrained guidance problems pertaining to missiles and UAVs. The first part of the thesis discusses a nonlinear guidance law for impact tim

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Abdul, Saleem P. K. "Guidance Laws for Engagement Time Control." Thesis, 2016. http://hdl.handle.net/2005/2926.

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Autonomous aerial vehicles like missiles and unmanned aerial vehicles (UAVs) have attracted various military and civilian applications. The primary guidance objective of any autonomous vehicle is to reach the desired destination point (target or waypoint). However, many practical engagements impose additional constraints like minimum control effort, a desired final velocity direction or a predefined engagement time. This thesis addresses engagement time constrained guidance problems pertaining to missiles and UAVs. The first part of the thesis discusses a nonlinear guidance law for impact tim

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38

Kumar, Shashi Ranjan. "Sliding Mode Control Based Guidance Strategies with Terminal Constraints." Thesis, 2015. http://etd.iisc.ac.in/handle/2005/3876.

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In the guidance literature, minimizing miss distance along with optimizing the energy usage had been an objective for several decades. In current day applications, additional terminal performance such as impact angle and impact time are of paramount importance. These terminal constraints increase warhead effectiveness and survivability of the interceptor. This thesis contributes to the design of guidance laws addressing terminal constraints such as impact angle, impact time, and both impact time as well as impact angle, in addition to interception of targets. In the first part of the thesis,

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Kumar, Shashi Ranjan. "Sliding Mode Control Based Guidance Strategies with Terminal Constraints." Thesis, 2015. http://etd.iisc.ernet.in/2005/3876.

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In the guidance literature, minimizing miss distance along with optimizing the energy usage had been an objective for several decades. In current day applications, additional terminal performance such as impact angle and impact time are of paramount importance. These terminal constraints increase warhead effectiveness and survivability of the interceptor. This thesis contributes to the design of guidance laws addressing terminal constraints such as impact angle, impact time, and both impact time as well as impact angle, in addition to interception of targets. In the first part of the thesis,

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40

Suresh, M. "UAV Group Autonomy In Network Centric Environment." Thesis, 2013. https://etd.iisc.ac.in/handle/2005/2596.

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It is a well-recognized fact that unmanned aerial vehicles are an essential element in today’s network-centric integrated battlefield environment. Compared to solo UAV missions, multiple unmanned aerial vehicles deployed in co-operative mode, offer many advantages that has motivated UAV researchers all over the world to evolve concept of operations that aims in achieving a paradigm shift from traditional ”dull” missions to perform ”dirty” and ”dangerous” missions. In future success of a mission will depend on interaction among UAV groups with no interaction with any ground entity. To reach th

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Suresh, M. "UAV Group Autonomy In Network Centric Environment." Thesis, 2013. http://etd.iisc.ernet.in/handle/2005/2596.

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It is a well-recognized fact that unmanned aerial vehicles are an essential element in today’s network-centric integrated battlefield environment. Compared to solo UAV missions, multiple unmanned aerial vehicles deployed in co-operative mode, offer many advantages that has motivated UAV researchers all over the world to evolve concept of operations that aims in achieving a paradigm shift from traditional ”dull” missions to perform ”dirty” and ”dangerous” missions. In future success of a mission will depend on interaction among UAV groups with no interaction with any ground entity. To reach thi

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