Gotowe bibliografie tematyczne / Missili cruise

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Gotowa bibliografia na temat „Missili cruise”

Autor: Grafiati

Data publikacji: 29 lipca 2024

Data aktualizacji: 30 lipca 2024

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Artykuły w czasopismach na temat "Missili cruise"

Bychkov, V. V. "Bychkov V. V. Strategic concept for the development of non-strategic missiles - sea-based complexes". National Security and Strategic Planning 2020, nr 4 (20.01.2021): 20–28. http://dx.doi.org/10.37468/2307-1400-2021-2020-4-20-28.

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The creation of a specific missile system with sea-based cruise missiles is determined by the principles of construction, solved goals and tasks. The priority areas for the development of promising missile weapons are factors such as: a combination of small weight and size character-istics of the missile and its area of an effective reflecting surface; optimization of flight altitude at cruise and final sections, at homing of cruise missiles on target; provision of antiosenitic ma-neuver and high speeds of cruise missiles flight to trajectories and much more.

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Yu, Yong Tao, i Ying Ding. "Application of Improved ANT Algorithm to Planning of Anti-Ship Cruise Missile Route". Advanced Materials Research 989-994 (lipiec 2014): 1747–50. http://dx.doi.org/10.4028/www.scientific.net/amr.989-994.1747.

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Anti-ship cruise missile (ASCM) attack route meets the needs of the attack mission will determine the effect of the subsequent attacks. According to research planning of anti-ship cruise missile route based on improved ANT algorithm by elitist strategy. The first is sensitive factor analysis of route planning based on operational requirements. Second is established an objective function and constraints set of route planning, achieved anti-ship cruise missile route planning model. Finally, based on specific objectives, situation and the user's strategies, it can use improved ANT algorithm to plan anti-ship cruise route.

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Wade, Brian M. "A multi-objective optimization of ballistic and cruise missile fire plans based on damage calculations from missile impacts on an airfield defended by an air defense artillery network". Journal of Defense Modeling and Simulation: Applications, Methodology, Technology 16, nr 2 (13.07.2018): 103–17. http://dx.doi.org/10.1177/1548512918788503.

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This paper presents a new methodology for optimizing missile fire plan parameters in order to maximize the damage caused to an airfield by the impacts of ballistic and cruise missiles that leak through an air defense artillery network using weaponeering calculations. This new methodology models the damage to the airfield runway, fuel infrastructure, and parked aircraft caused by both unitary and submunition warheads carried by the ballistic and cruise missiles. It then uses the airfield damage models paired with an air defense simulation in a multi-objective optimization to find the non-dominated frontier of missile fire plan parameters that inflict the greatest damage to the different parts of the defended airfield. It demonstrates the methodology for three increasingly sized ballistic and cruise missile fire plans.

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Fuzhen, Shi, Guo Jinrui i Ren Mingze. "Optimization Design of the Wing of Cruise Missile on the Basis of the Vortex Lattice Approach". Journal of Physics: Conference Series 2457, nr 1 (1.03.2023): 012034. http://dx.doi.org/10.1088/1742-6596/2457/1/012034.

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Abstract Aerodynamic performance of missile wings is a vital factor affecting the endurance and combat effectiveness of cruise missiles. Given the current situation that the aerodynamic design of conventional cruise missile wings is less and there is more room for improvement, a missile wing shape with a winglet is considered designed to improve the cruise characteristics of cruise missiles effectively. Firstly, the EPPLER 66 is selected as the wing shape by the combination of vortex surface element approach batch calculation and CFD simulation analysis. According to the dimensional parameters of a typical patrol wing, the design variables and corresponding optimization intervals are determined, and the aerodynamic optimization is carried out by combining the genetic approach as well as the vortex lattice approach. CFD is used to verify the aerodynamic performance of the optimized wing. The calculation outcomes reveal that the optimized wing has a ratio of lift-to-drag of 23.43, which is 12.32% higher than that of the conventional flat wing.

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Pereira, Carolina Almeida, Joana Moreira Ferreira, Francini Monteiro Costa i Cristiana Guedes Oliveira. "A importância do LinkedIn nas estratégias de assessoria em turismo: estudo de caso de oito marcas de cruzeiros turísticos". Prisma.com 43 (2020): 130–57. http://dx.doi.org/10.21747/16463153/43a7.

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This work aims to understand the role that press office have and relate it with the importance of the social network, LinkedIn in press office tourism strategies. As such, a study case that involves eight brands related to cruises has been developed: Celebrity Cruises, Royal Caribbean International, Norwegian Cruise Line, Carnival Cruises, Princess Cruises, Holland America Line, MSC Cruises e Costa Cruises. In this way, we want to understand the impact that communication has on social media, especially on LinkedIn and on his mission. With this study, we conclude that LinkedIn is used as a platform of networking, marketing and public relations of people and companies, and denotes an increasing popularity.

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Munchak, Volodymyr, Oleksandr Vysikan, Oleksii Stepaniuk i Yurii Maznychenko. "TO THE STUDY OF STRATEGIC CRUISE MISSILES X-101". Criminalistics and Forensics, nr 68 (3.07.2023): 715–30. http://dx.doi.org/10.33994/kndise.2023.68.70.

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According to existing provisions, the examination of missile weapons is a set of expert research activities aimed at studying missile and jet weapons, as well as their components (mechanisms, assemblies, etc.) and their interaction in order to obtain reliable information about the objects provided for research. The article discusses some aspects of the research of missile weapons – strategic cruise missiles X-101, the relevance of which is due to their constant use in russia. Now russia is again carrying out massive missile strikes against Ukraine with X-101/55 missiles. The occupiers have changed tactics and prefer mainly strategic cruise missiles to destroy military installations and infrastructure. At the same time, it should be borne in mind that until now there is no methodology for conducting an examination of artillery and missile weapons, and in the specialized literature there is only distinguishable data on missile weapons. Based on the generalization of the expert research practice of the Explosive Research and Research of Rocket and Artillery Weapons Department of the Military Research Laboratory of the Kyiv Scientific Research Institute of Forensic Expertise, the structural features of the X-101 strategic cruise missile were determined. Considering that many experts do not have information on these missiles, the material of this article will be used in the examination of missile weapons, namely, in the identification and description of research objects. A missile weapons examination is a qualification examination, during which not only an object can be identified as a missile weapon, but it can also be determined what type or type of missile weapon the object belongs to, as well as how this weapon was manufactured. The examination of missile weapons requires special knowledge in the field of missile and jet weapons (the structure/design features and properties of weapons, the procedure for handling and using them, ammunition for them, and the consequences of using them).

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Miskolczi, Márk, i Melinda Jászberényi. "Szállodahajó-turizmus a Dunán – trendek és termékfejlesztési lehetőségek Cruise tourism on the Danube – trends and product development opportunities". Turizmus Bulletin 21, nr 1 (kwiecień 2021): 13–25. http://dx.doi.org/10.14267/turbull.2021v21n1.2.

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Napjaink gyorsan változó fogyasztói trendjei folyamatos megújulásra ösztönzik a turizmuságazat szereplőit. A dunai szállodahajó-turizmus a szabadidős célú turisztikai utazások feltörekvő részterülete, ugyanakkor a hosszú távon is kiemelkedő gazdasági teljesítmény fenntartásához szükség van a termékkonstrukció időszakos megújítására. Jelen tanulmány a dunai szállodahajóturizmus alapismérveit, piaci (keresleti-kínálati) jellemzőit foglalja össze a témakörben publikált folyóiratcikkek elemzésén keresztül. Bemutatja továbbá a piacvezető vállalatok (Tauck, Avalon Waterways, Crystal Cruises, Uniworld River Cruises, Viking River Cruises, Scenic River Cruises) aktuális (2020-2022-re szóló) termékkínálatát. A kvalitatív kutatás során 326 utazási csomag áttekintésére került sor, mely rámutatott a kulturális turisztikai attrakciók termékkínálatban betöltött kiemelkedő szerepére. Az eredmények alátámasztják, hogy számos turisztikai termék (például: természeti vonzerők, egészség- és gyógyturizmus) hiányzik a jelenlegi termékkonstrukcióból, melyeknek a kínálatba történő beépítése elősegítheti a célcsoport bővítését, ami a recesszió utáni időszakban hozzájárulhat a dunai szállodahajózás gazdasági teljesítményének javulásához. Tourism is shaped by rapidly changing consumer trends. Cruise tourism on the Danube is an emerging part of leisure tourism, but at the same time, to maintain outstanding economic performance in the long run, it is necessary to periodically renew the product portfolio. The following study summarizes the basic characteristics and market (supply-demand) features of Danube cruise tourism by a systematic literature review. The study presents the current (2020-2022) supply of market-leading companies (Tauck, Avalon Waterways, Crystal Cruises, Uniworld River Cruises, Viking River Cruises, Scenic River Cruises) by content analysis. Using qualitative research, 326 travel packages were reviewed, in which the dominant role of cultural tourist attractions was clear. The results confirm that many tourism products (e.g., natural attractions, medical tourism) are missing from the product range. Their addition could improve the economic performance of Danube cruise tourism in the post-recession period by expanding the target group.

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Kovalev, M. A., i A. N. Nikitin. "Choosing the aerodynamic configuration of a subsonic cruise missile". VESTNIK of Samara University. Aerospace and Mechanical Engineering 18, nr 3 (31.10.2019): 59–66. http://dx.doi.org/10.18287/2541-7533-2019-18-3-59-66.

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The paper presents a comparison of two aerodynamic configurations of subsonic cruise missiles, characterized by the use of swept-back and forward-swept wings. The results of wind tunnel tests with the use of an automated measurement system characterizing the dependence of the lift and drag coefficients in a sufficiently wide range of angles of attack are presented. This allows us to compare the aerodynamic quality of the cruise missile models under investigation. The analysis of the results of experiments with the models and calculations in conditions of steady-state low-altitude horizontal flight revealed that the configurations of cruise missiles with a moderately swept wing, selected for comparison, have similar aerodynamic characteristics. Both configurations ensure the mode of flight at a given altitude and velocity in the range of the best angles of attack (maximum aerodynamic quality). Missiles with swept-back wings have better aerodynamic performance in terms of maximum aerodynamic quality, while the lift increment due to reduced trim losses for the forward-swept wing configuration only partially compensates the difference of the aerodynamic characteristics of the alternatives under consideration. Therefore, it is concluded that the choice of aerodynamic configuration of a subsonic cruise missile with a swept-back wing is preferable.

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Voloshchenko, Oleksandr, Vitalii Kosenko, Oleksandr Kovbasa, Ihor Chernykh i Illia Kaplia. "Methodical approach to determining the resistance of field fortification coating structures built to the shock-explosive impact of modern missile weapons". Strength of Materials and Theory of Structures, nr 111 (24.11.2023): 178–87. http://dx.doi.org/10.32347/2410-2547.2023.111.178-187.

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The purpose of the article is to publicize a methodical approach to determining the stability of cover structures of field fortifications to the shock-explosive action of modern missile weapons, in particular cruise and ballistic missiles. The purpose of this article is to present a methodological approach for determining the resistance of the cover structures of field fortifications to the impact and explosive effects of modern missile weapons, in particular cruise and ballistic missiles.The analysis shows that currently, the most dangerous means of fire destruction for troops are long-range cruise and ballistic missiles with high explosive effect. Under such conditions, the most effective way to protect troops is to shelter them in field fortifications, the cover structures of which are resistant to the impact and explosive effects of these missiles.The article presents a methodological approach to determining the resistance of the cover structures of field fortifications to the impact and explosive effects of cruise and ballistic missiles and the results of determining the required thickness of the cover of these structures, which are made of the most readily available building materials in the field – soil, sand, clay, stone, concrete and reinforced concrete. The scientific novelty of the proposed methodological approach lies in the comprehensive consideration of a set of indicators quantifying the main tactical and technical characteristics of modern cruise and ballistic missiles, their flight and trajectory parameters, as well as indicators taking into account the most important properties of materials for the construction of a penetration and emission protection cover of a field fortification.

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Mistry, Dinshaw, i Mark Smith. "Negotiating Multilateral Instruments Against Missile Proliferation". International Negotiation 10, nr 3 (2005): 425–51. http://dx.doi.org/10.1163/157180605776087480.

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AbstractThe absence of a major multilateral treaty banning missiles is explained by the limited scope of the two main instruments against missile proliferation – the Missile Technology Control Regime (MTCR) and the Hague Code of Conduct against Ballistic Missile Proliferation (HCOC). In the MTCR's case, limiting the scope to supply-side technology controls facilitated progress during its negotiations. In the Hague Code, limiting the scope to transparency, and keeping out additional items such as incentives to renounce ballistic missiles and the topic of cruise missiles, made negotiations easier. The trade-off from a limited scope in both instruments is that there is still no significant worldwide treaty banning missiles.

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Rozprawy doktorskie na temat "Missili cruise"

Bircan, Gokhan. "Cruise Missile Mission Rehearsal". Master's thesis, METU, 2011. http://etd.lib.metu.edu.tr/upload/12613948/index.pdf.

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Cruise missile mission planning is a key activity of cruise missile operations. Ground planning activities aim at low observable missions that have high probability of success. These activities include end game planning, route planning and launch planning. While end game planning tries to optimize end game parameters for maximum effectiveness, route planning tries to maximize survivability and enable navigational supports by determining the waypoints to from launch zone to target through a defended area. And lastly, planner tries to find the appropriate launch parameters that will prohibit platform to contact enemy agents. Mission rehearsal is the execution of the planned mission in a virtual environment that will be constructed with the data that drives the planning process. Mission rehearsal will support planners by providing possible results of the planned mission. Stochastic processes of the execution of the planned mission will be incorporated in the simulation of the combat. Along with platform, cruise missile and target, other players like SAM Sites or Search Radars (Early Warning Radars) will be incorporated in the rehearsal process.

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Sparks, Timothy F. "The dawn of cruise missile diplomacy". Monterey, Calif. : Springfield, Va. : Naval Postgraduate School ; Available from National Technical Information Service, 1997. http://handle.dtic.mil/100.2/ADA333251.

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Thesis (M.A. in National Security Affairs) Naval Postgraduate School, June 1997.
Thesis advisors, Peter R. Lavoy, Cynthia J. Levy. Includes bibliographical references (p. 61-64). Also Available online.

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Gauthier, Kathryn L. "AIRBORNE TELEMETRY AND CRUISE MISSILE CONTROL". International Foundation for Telemetering, 1985. http://hdl.handle.net/10150/615744.

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International Telemetering Conference Proceedings / October 28-31, 1985 / Riviera Hotel, Las Vegas, Nevada
The Advanced Range Instrumentation Aircraft (ARIA) is an airborne platform designed to receive, record, process, and retransmit telemetry data. This paper will provide a brief overview of ARIA capabilities and focus on a specially modified ARIA – the Cruise Missile Mission Control Aircraft (CMMCA). Currently utilized in cruise missile testing, CMMCA features on-board real-time display of telemetry data as well as remote command and control of the test missile.

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Kuykendall, Scott D. "Optimizing selection of Tomahawk Cruise Missiles". Thesis, Monterey, Calif. : Springfield, Va. : Naval Postgraduate School ; Available from National Technical Information Service, 1998. http://handle.dtic.mil/100.2/ADA344719.

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Thesis (M.S. in Operations Research) Naval Postgraduate School, March 1998.
"March 1998." Thesis advisor(s): Richard E. Rosenthal. Includes bibliographical references (p. 39). Also available online.

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Le, Voyer Damien. "Guidance and Control of a Naval Cruise Missile". Thesis, KTH, Reglerteknik, 2008. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-105890.

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Today the armed forces of many countries need to strike accurately potential enemies, wherever they might be, from a safe place. Since naval units can be deployed almost everywhere in the open sea, the idea of a naval cruise missile emerged in the 70’s. These missiles are designed to be launched from various naval vehicles such as frigates or submarines and strike deeply in the enemy territory. A program called Missile de Croisière Naval (MdCN Naval Cruise Missile) was therefore launched in 2006 by the DGA, the French procurement agency. MBDA is the industrial company appointed by the DGA to design and build the missile. Control aspects on a cruise missile are of primary interest since they impact the reliability, performance and availability of the weapon. In the aeronautics and weapon industry, gain scheduled controllers are used in most cases. However, many non-linear techniques have been developed in the literature and might improve the behaviour of the missile. The main objective of the present thesis is to apply non-linear techniques on the control and guidance loops of the MdCN too see whether of not they can improve such a system. Based on this report it should be easy for the engineers of the DGA to compare the controllers of the thesis and the classical gain scheduled controllers used in the industry. To achieve this task some basic knowledge of flight dynamics are recalled and a model of the MdCN is computed and divided into the control loop and the guidance loop. Then a non-linear controller for the launch phase using a Lyapunov based technique called back-stepping is designed and tested through a statistic analysis. During the cruise phase different anti-windup strategies are applied on the propulsion control loop of the missile and compared. Finally a software interface with a navigation-dedicated tool is coded and implemented in Simulink to analyse the complete Guidance-Navigation-Control loop and to see how navigation errors impact the control algorithms. The main contributions of this thesis are the controllers designed for the launch phase and the propulsion loop that will be compared with the controller that MBDA is going to deliver next year to see whether or not the non-linear techniques used in the thesis should be used on the missile. Furthermore, all the tools and procedure set up to interface the control and guidance laws with the navigation models and filters will give the possibility to the DGA to have a deeper understanding of the algorithms used by MBDA and to make sure that navigation and estimation issues are properly taken in account when designing the control and guidance laws.

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Dowling, William M. Soria Javier C. "Optimizing Ground Based Air Defense in support of homeland defense the cruise missile threat /". Monterey, Calif. : Naval Postgraduate School, 2006. http://bosun.nps.edu/uhtbin/hyperion.exe/06Dec%5FDowling.pdf.

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Thesis (M.S. in Defense Analysis)--Naval Postgraduate School, December 2006.
Thesis Advisor(s): Frank Giordano. "December 2006." Includes bibliographical references (p. 71-73). Also available in print.

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Ekutekin, Vedat. "Navigation And Control Studies On Cruise Missiles". Phd thesis, METU, 2007. http://etd.lib.metu.edu.tr/upload/12608142/index.pdf.

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A cruise missile is a guided missile that uses a lifting wing and a jet propulsion system to allow sustained flight. Cruise missiles are, in essence, unmanned aircraft and they are generally designed to carry a large conventional or nuclear warhead many hundreds of miles with excellent accuracy. In this study, navigation and control studies on cruise missiles are performed. Due to the variety and complexity of the subsystems of the cruise missiles, the main concern is limited with the navigation system. Navigation system determines the position, velocity, attitude and time solutions of the missile. Therefore, it can be concluded that an accurate self-contained navigation system directly influences the success of the missile. In the study, modern radar data association algorithms are implemented as new Terrain Aided Navigation (TAN) algorithms which can be used with low-cost Inertial Measurement Units (IMU&rsquo
s). In order to perform the study, first a thorough survey of the literature on mid-course navigation of cruise missiles is performed. Then, study on modern radar data association algorithms and their implementations to TAN are done with simple simulations. At the case study part, a six degree of freedom (6 DOF) flight simulation tool is developed which includes the aerodynamic and dynamic model of the cruise missile model including error model of the navigation system. Finally, the performances of the designed navigation systems with the implemented TAN algorithms are examined in detail with the help of the simulations performed.

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Chichka, David F. "Cruise-dash optimization applied to an air-breathing missile". Thesis, Virginia Polytechnic Institute and State University, 1985. http://hdl.handle.net/10919/90923.

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The method of singular perturbations is applied to the determination of the optimal range-fuel-time trajectory for an air-breathing missile. This method is shown to lead to the reduced-order "cruise-dash" model, and this model is used in the optimization study. Earlier work in this area is extended by the inclusion of two not heretofore considered limits on the dynamical system. The results of the earlier work are shown to hold throughout much of the velocity regime in which the missile operates, but operation in the very high and very low velocity ranges is shown to be sharply curtailed, with the optimal operating points being changed drastically in some cases. Also, the effect of the non-zero minimum admissible throttle setting and the resultant throttle-chattering on the solution of the control problem is examined in some detail.
M.S.

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Camacho, Juan G., Lawrence F. Guest, Belen M. Hernandez, Thomas M. Johnson, Alan H. Kang, Giang T. Le, Brian J. MacGillivray, Tu K. Ngo, Kyle B. Norman i Franklin Tomei. "Open architecture as an enabler for FORCEnet Cruise Missile Defense". Thesis, Monterey, California. Naval Postgraduate School, 2007. http://hdl.handle.net/10945/6930.

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Advancements in missile technology have made cruise missile capability available worldwide. Current US naval weapon systems lack full interoperability across multiple platforms and full integration of detection, control, and engagement processes against incoming targets. The key to defeating future threats to our military assets is in gaining additional reaction time. This can be accomplished by leveraging collective sensor detection data throughout the battlespace, utilizing the FORCEnet data resources to evaluate the threat, and engaging the threat with a tiered defense. The objective of this capstone project is to address the above issues through the use of Open Architecture (OA) within a FORCEnet environment. This report focuses on the development of a conceptual architecture for Cruise Missile Defense (CMD) that combines FORCEnet architecture requirements with Program Executive Office of Integrated Warfare Systems (PEO IWS)'s OA functional architecture technical requirements. Further, this conceptual architecture is compared with PEO IWS's functional architecture via a series of systems engineering diagrams. These diagrams culminate in a simulation model that analyzes and determines the validity of the conceptual architecture. Results from the simulation model show that the conceptual architecture performed significantly better than PEO IWS's. These results are attributed to the addition of a re-engagement loop called Observe-Orient-Decide-Act (OODA).

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Jones, Antonio T. "Long-range precision-strike cruise missiles inNATO operations". Thesis, Monterey, California: Naval Postgraduate School, 2014. http://hdl.handle.net/10945/41399.

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Approved for public release; distribution is unlimited.
In 1949, NATO was established as a military alliance organized to protect its members from aggression or coercion by its adversaries to the East. However, after the collapse of the Soviet Union, the geostrategic context for NATO transformed significantly, with a new set of security threats (ethnic conflicts, terrorism, nuclear proliferation, organized crime, etc.). For NATO to remain relevant, its members had to sustain its overall purpose of collective defense and contribute to collective security in the post-Cold War world, in which several internal and external factors have transformed. While the Alliance remains a collective defense organization, the Allies have nonetheless assumed additional roles in conflict prevention and crisis management. In its crisis management role, advances in military technology have afforded NATO the opportunity to utilize a significant strategic weapon, the Tomahawk Land Attack Missile (TLAM). For NATO, the TLAM has demonstrated its utility for specific purposes; and it has transformed the landscape of modern warfare. This weapon has allowed NATO to enhance its force projection capability, while minimizing risks for Alliance personnel (aircrews and ground troops) when conducting strike operations.

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Książki na temat "Missili cruise"

Centre for Air Power Studies (New Delhi, India), red. Cruise missiles: Evolution, proliferation, and future. New Delhi: KW Publishers in association with Centre for Air Power Studies, 2011.

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Canadian Institute for International Peace and Security., red. The Cruise missile and cruise missile testing in Canada. Ottawa, Ont: Canadian Institute for International Peace and Security, 1988.

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Curren, Thomas. Cruise missiles. [Ottawa]: Library of Parliament, Research Branch, 1989.

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Larson, Eric V. Technological risk: The case of the Tomahawk cruise missile. Santa Monica, CA: Rand, 1990.

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Lempert, Robert J. Cruise missile arms control. Santa Monica, CA: Rand Corp., 1989.

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International Institute for Strategic Studies., red. Dealing with the threat of cruise missiles. Oxford: Oxford University Press, 2001.

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Gottemoeller, Rose E. Land-attack cruise missiles. London: International Institute for Strategic Studies, 1987.

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Werrell, Kenneth P. The evolution of the cruise missile. Maxwell Air Force Base, Ala: Air University, Air University Press, 1997.

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Werrell, Kenneth P. The evolution of the cruise missile. Maxwell Air Force Base, Ala: Air University, Air University Press, 1985.

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Carek, David A. Structural analysis of high-rpm composite propfan blades for a cruise missle wind tunnel model. [Washington, DC: National Aeronautics and Space Administration, 1993.

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Części książek na temat "Missili cruise"

Naresh Kumar, G., Shweta Dadarya, Akshay Verandani, A. K. Sarkar i S. E. Talole. "Cruise Missile Mission Planning Using Genetic Algorithm". W Lecture Notes in Mechanical Engineering, 353–62. Singapore: Springer Singapore, 2018. http://dx.doi.org/10.1007/978-981-10-5849-3_34.

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Ghoshal, Debalina. "Technological Aspects of Missile: Missiles and Warheads". W Role Of Ballistic And Cruise Missiles In International Security, 19–31. Cham: Springer International Publishing, 2023. http://dx.doi.org/10.1007/978-3-031-48063-8_2.

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Wittlinger, Sandra, i Alexis Papathanassis. "‘Missing in (Cruise-) Action’: Exploring Missing Passenger Incidents on Board Cruise Ships". W Tourism, Hospitality & Event Management, 19–27. Cham: Springer International Publishing, 2018. http://dx.doi.org/10.1007/978-3-319-94664-1_2.

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Gottemoeller, Rose. "Verifying Controls on Cruise Missiles". W Verification and Compliance, 17–44. London: Palgrave Macmillan UK, 1988. http://dx.doi.org/10.1007/978-1-349-10143-6_2.

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Thomas, Valerie. "Verification of Sea-Launched Cruise Missiles". W Verification of Arms Reductions, 38–47. Berlin, Heidelberg: Springer Berlin Heidelberg, 1989. http://dx.doi.org/10.1007/978-3-642-46684-7_5.

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Ghoshal, Debalina. "Why States Desire for Missile Systems?" W Role Of Ballistic And Cruise Missiles In International Security, 51–68. Cham: Springer International Publishing, 2023. http://dx.doi.org/10.1007/978-3-031-48063-8_4.

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Tsipis, Kosta. "Nuclear Cruise Missiles: The Problem of Verification". W The Arms Race in an Era of Negotiations, 100–114. London: Palgrave Macmillan UK, 1991. http://dx.doi.org/10.1007/978-1-349-11967-7_7.

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Ghoshal, Debalina. "Survivability of Nuclear Missile Forces and Contemporary Debates". W Role Of Ballistic And Cruise Missiles In International Security, 145–61. Cham: Springer International Publishing, 2023. http://dx.doi.org/10.1007/978-3-031-48063-8_6.

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Jobanputra, Ami, Dhruv Panchal, Het Trivedi, Dhyey Buch i Bhavin Kakani. "Development of Antennas Subsystem for Indian Airborne Cruise Missile". W Proceedings of the International Conference on Paradigms of Computing, Communication and Data Sciences, 619–29. Singapore: Springer Singapore, 2021. http://dx.doi.org/10.1007/978-981-15-7533-4_49.

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Ghoshal, Debalina. "Can the World Do Without Missiles?" W Role Of Ballistic And Cruise Missiles In International Security, 163–76. Cham: Springer International Publishing, 2023. http://dx.doi.org/10.1007/978-3-031-48063-8_7.

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Streszczenia konferencji na temat "Missili cruise"

Romanov, V. I., O. G. Zhiritsky, A. V. Kovalenko i V. V. Lupandin. "M21 Cruise Marine Combined Cycle Plant". W ASME 1995 International Gas Turbine and Aeroengine Congress and Exposition. American Society of Mechanical Engineers, 1995. http://dx.doi.org/10.1115/95-gt-450.

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The paper describes M21 cruise marine combined cycle plant for SLAVA class cruisers (COGAG arrangement). Three guided missile cruisers (Figure 1) are powered by these plants (two plants for each cruiser). During this plant development the more strict demands on weight and size had been taken into account as compared with M25 plants for merchant ships. The paper shows technical data of M21 combined cycle plant, descriptions and design features of SPA MASHPROEKT GT 6004R gas turbine with reversible free power turbine, waste-heat recovery boiler, steam turbine with a condenser and a common gear unit. More than 10 year service experience of these plants is shown in this paper.

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"Cruise Missile". W Planet Austria. Wien: Verlag der Österreichischen Akademie der Wissenschaften, 2009. http://dx.doi.org/10.1553/planetaustrias164.

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Edefur, Henrik, Fredrik Haglind i Stefan Olsson. "Design of an Air-Launched Tactical Missile for Three Different Propulsion Systems: ATR, Rocket and Turbojet". W ASME Turbo Expo 2007: Power for Land, Sea, and Air. ASMEDC, 2007. http://dx.doi.org/10.1115/gt2007-27844.

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The objective of this paper is to assess the feasibility of a solid propellant Air Turbo Rocket (ATR), in comparison with a conventional turbojet engine or a solid rocket motor, as power source for a medium range tactical air-launched missile from an overall system point of view. A sizing method for missiles is developed, which together with flight performance calculations and engine performance data determines the final size and weight of the missile and its engine. The results suggest that an ATR engine is more favourable than a jet engine when the ratio between maximum (manoeuvre) thrust and minimum (cruise) thrust is large; for example for a mission including a cruise segment and a high load factor manoeuvre made at constant speed. For the missile range investigated in this paper no breakpoint in distance has been found beyond which the ATR engine becomes impractical. The rocket motor can produce a huge amount of thrust, thus giving it a very large maximum to minimum thrust ratio. However, it has a disadvantage in its low fuel efficiency and high combustion temperature, making it impracticable for missions requiring any longer duration. Altogether the choice of propulsion system has a large impact on maximum take-off weight, size and performance of the missile.

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Seigler, T. Michael, Jae-Sung Bae i Daniel J. Inman. "Flight Control of a Variable Span Cruise Missile". W ASME 2004 International Mechanical Engineering Congress and Exposition. ASMEDC, 2004. http://dx.doi.org/10.1115/imece2004-61961.

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In this work the benefits of variable span morphing are considered, specifically with regards to the increased maneuverability of bank-to-turn cruise missiles. Along with an increase in range associated with variable span aircraft-in the case where both wings are equally extended-there is also the possibility of an additional advantage of higher control authority over both pitch and roll motions. In the case of roll control, one wing is extended while the other is contracted thus producing a moment about the longitudinal axis of the missile. Compared to conventional tail surface control, this moment can be substantial depending on the flight conditions. There is, however, some complexity involved in flight control of variable span aircraft; namely the shift of the missile’s center of mass and the dependence of the roll producing moment on the angle of attack. The following work attempts to address these complexities through nonlinear control. First, a full nonlinear model of the missile is presented that includes aerodynamic effects and changes in weight distribution. Nonlinear methods are then used to control the trajectory of the missile via the roll angle, angle of attack, and sideslip angle. The results show that, in comparison with conventional missile configurations, the addition of variable span morphing has the capability of increasing overall flight performance.

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Waldemark, Joakim T. A., Vlatko Becanovic, Thomas Lindblad, Clark S. Lindsey, Karina E. Waldemark i Jason M. Kinser. "Pulse-coupled neural networks for cruise missile guidance and mission planning". W Ninth Workshop on Virtual Intelligence/Dynamic Neural Networks: Neural Networks Fuzzy Systems, Evolutionary Systems and Virtual Re, redaktorzy Thomas Lindblad, Mary Lou Padgett i Jason M. Kinser. SPIE, 1999. http://dx.doi.org/10.1117/12.343034.

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Yan, Daiwei, Lei Pan i Liangxian Gu. "Estimation the Mission Effectiveness of Hypersonic Cruise Missile in Conceptual Design". W 46th AIAA Aerospace Sciences Meeting and Exhibit. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2008. http://dx.doi.org/10.2514/6.2008-176.

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PAGE, DON, FRED GLOYNA i DAVID EARLS. "Environmental mission profile facility for reliability testing of multiple cruise missile electronic boxes". W 28th Joint Propulsion Conference and Exhibit. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1992. http://dx.doi.org/10.2514/6.1992-3893.

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Blankson, Isaiah M. "Air-Breathing Hypersonic Cruise: Prospects for Mach 4-7 Waverider Aircraft". W ASME 1992 International Gas Turbine and Aeroengine Congress and Exposition. American Society of Mechanical Engineers, 1992. http://dx.doi.org/10.1115/92-gt-437.

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There is currently a renewal of world-wide interest in hypersonic flight. Vehicle concepts being considered range from cruise missiles to SSTO and TSTO vehicles. The new characteristics of these vehicles are that they will be powered by air-breathing engines and have long residence times in the air-breathing corridor. In the Mach 4-7 regime, waverider aircraft are being considered as candidates for both long-range and short-range cruise missions, as hypersonic missiles, and as high L/D highly maneuverable vehicles. This paper will discuss the potential for near-term and far-term application of air-breathing engines to the above waverider vehicle concepts and missions. In particular, the cruise mission is discussed in detail and attempts are made to compare and contrast it with the accelerator mission. Past criticisms levied against waveriders alleged low volumetric efficiency, lack of engine/airframe integration studies, poor off-design performance, poor take-off and landing capability, have been shown by on-going research to be unfounded. A discussion is presented of some of the technical challenges and on-going research aimed at realizing such vehicles: from turboramjet and scramjet technology development, propulsion-airframe integration effects on vehicle performance, aeroservothermoelastic systems analysis, hypersonic stability and control with aeroservothermoelastic and propulsion effects, etc. A unique and very strong aspect of hypersonic vehicle design is the integration and interaction of the propulsion system, aerodynamics, aerodynamic heating, stability and control, and materials and structures. This first-order multidisciplinary situation demands the ability to integrate highly-coupled and interacting elements in a fundamental and optimal fashion to achieve the desired performance. Some crucial technology needs are found in propulsion-airframe integration and its role in configuration definition, hypersonic boundary-layer transition and its impact on vehicle gross-weight and mission success, scramjet combustor mixing length and its impact on engine weight and, CFD (turbulence modeling, transition modeling, etc) as a principal tool for the design of hypersonic vehicles. Key technology implications in thermal management, structures, materials, and flight control systems will also be briefly discussed. It is concluded that most of the technology requirements in the Mach 4-7 regime are relatively conventional making cited applications near-term, yet offering very significant advancements in aircraft technology.

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Nugroho, Gesang, Yarabisa Yanuar i Praberta Ardi Wibowo. "Flight Test of Pasopati Electrical Cruise Missile". W 2019 International Conference on Advanced Mechatronics, Intelligent Manufacture and Industrial Automation (ICAMIMIA). IEEE, 2019. http://dx.doi.org/10.1109/icamimia47173.2019.9223373.

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Bemrose, Travis, i Rodney Andree. "Computer-Based Cruise Missile Trainer for Nuclear WSEP". W 2007 U.S. Air Force T&E Days. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2007. http://dx.doi.org/10.2514/6.2007-1625.

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Raporty organizacyjne na temat "Missili cruise"

Brockmann, Kolja, i Dmitry Stefanovich. Hypersonic Boost-Glide Systems and Hypersonic Cruise Missiles: Challenges for the Missile Technology Control Regime. Stockholm International Peace Research Institute, kwiecień 2022. http://dx.doi.org/10.55163/bdyx5243.

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An increasing number of states are pursuing hypersonic missile development programmes, including for hypersonic boost-glide systems and hypersonic cruise missiles. Hypersonic missiles combine hypersonic speed and manoeuvrability which can result in target ambiguity, render missile defences ineffective and reduce warning times. Some hypersonic missiles are developed as delivery systems both for nuclear and conventional payloads. The combination of these capabilities may have escalatory or destabilizing effects. The Missile Technology Control Regime (MTCR) is the main instrument through which states seek to harmonize export control policies to govern the transfer of missile technology. It is key to ensure that the MTCR’s guidelines and control list adequately cover hypersonic missiles and related goods and technologies. This paper seeks to improve the understanding of hypersonic missiles, increase awareness among policy makers and export control officials, and inform the ongoing technical and policy discussions within the MTCR to strengthen efforts to limit the proliferation of hypersonic missiles.

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Dunbar, William G., i Sidney W. Silverman. Cruise Missile Power System. Fort Belvoir, VA: Defense Technical Information Center, marzec 1986. http://dx.doi.org/10.21236/ada174324.

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Tissue, Phil, Ron Perkins, Darren Sawyer i Lyle Powell. Attacking the Cruise Missile Threat. Fort Belvoir, VA: Defense Technical Information Center, wrzesień 2003. http://dx.doi.org/10.21236/ada421607.

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Werrell, Kenneth P. The Evolution of the Cruise Missile. Fort Belvoir, VA: Defense Technical Information Center, wrzesień 1985. http://dx.doi.org/10.21236/ada162646.

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Maloney, Michael S. Cruise Missile Attack Are We Prepared. Fort Belvoir, VA: Defense Technical Information Center, marzec 2007. http://dx.doi.org/10.21236/ada469582.

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Woodside, Robert E., John McIver, Daniel Gadler, James Beyar i James Howe. Feasibility of Third World Advanced Ballistic and Cruise Missile Threat. Volume 2: Emerging Cruise Missile Threat. Fort Belvoir, VA: Defense Technical Information Center, czerwiec 2000. http://dx.doi.org/10.21236/ada377356.

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Sivakumaran, N. S., Paul A. Bigelman, Laura T. Lee i Robert J. Jesionowski. The Probability of Negation of a Cruise Missile,. Fort Belvoir, VA: Defense Technical Information Center, listopad 1998. http://dx.doi.org/10.21236/ada357518.

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Noone, Emily, i Lydia Harriss. Hypersonic missiles. Parliamentary Office of Science and Technology, czerwiec 2023. http://dx.doi.org/10.58248/pn696.

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This POSTnote looks at hypersonic missile technologies, efforts to develop them, potential applications, and the possible challenges they may present for missile defence and global stability. Key Points: • Hypersonic missiles combine speeds of over five times the speed of sound with significant manoeuvrability during flight. • Their manoeuvrability enables them to change trajectory during flight, making their flight-path and target difficult to predict. • They fly at lower altitudes than ballistic missiles, which means that they may be harder to track at long distances with some surface-based sensors, such as certain radar. • There are two main types of hypersonic missile: hypersonic glide vehicles (HGVs) and hypersonic cruise missiles (HCMs). • HGVs are mounted onto rocket boosters for launch and may be accelerated to speeds of Mach 20 or more. The glider then separates from the booster and flies unpowered in the Earth’s upper atmosphere at altitudes of 30-80 km, before diving towards the target. • HCMs typically have a ramjet or scramjet engine that enables them to reach hypersonic speeds at altitudes of 20-40 km. • China and Russia have reportedly deployed hypersonic missiles that could deliver conventional or nuclear weapons. The US is testing multiple hypersonic technologies. • The AUKUS agreement between the UK, US and Australia includes developing hyper-sonic and counter-hypersonic technologies. • Developing hypersonic missiles requires significant research and development challenges to be overcome, contributing to their high development and manufacturing costs. • The speed, manoeuvrability and altitude of hypersonic missiles may challenge existing missile defences, although their uses and effectiveness are still being assessed. • Defence analysts disagree about the potential implications of hypersonic missiles for global peace and stability. Some suggest they could increase the risk of conflict escalation, while others say that they will not alter the strategic balance between nuclear powers. • Arms control, export controls and other measures may help limit potential harm to peace and stability, but these approaches face challenges.

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Dale, C. J. Naval Arms Control: The Sea Launched Cruise Missile Debate. Fort Belvoir, VA: Defense Technical Information Center, luty 1990. http://dx.doi.org/10.21236/ada437745.

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Crupper, Jr, McDonald Charles G. i Richard T. The Ground-Launched Cruise Missile in NATO: Political Aspects. Fort Belvoir, VA: Defense Technical Information Center, kwiecień 1988. http://dx.doi.org/10.21236/ada192610.

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