Log in

Relevant bibliographies by topics / Missile Impact / Journal articles

To see the other types of publications on this topic, follow the link: Missile Impact.

Journal articles on the topic 'Missile Impact'

Author: Grafiati

Published: 3 June 2025

Last updated: 31 July 2025

Create a spot-on reference in APA, MLA, Chicago, Harvard, and other styles

Select a source type:

Consult the top 50 journal articles for your research on the topic 'Missile Impact.'

Next to every source in the list of references, there is an 'Add to bibliography' button. Press on it, and we will generate automatically the bibliographic reference to the chosen work in the citation style you need: APA, MLA, Harvard, Chicago, Vancouver, etc.

You can also download the full text of the academic publication as pdf and read online its abstract whenever available in the metadata.

Browse journal articles on a wide variety of disciplines and organise your bibliography correctly.

1

Tianyang, Zhang, Zhang Jiahao, and Yu Qingbo. "Research on aerodynamic optimization of hypersonic missiles." Journal of Physics: Conference Series 2891, no. 11 (2024): 112026. https://doi.org/10.1088/1742-6596/2891/11/112026.

Full text

Abstract:

Abstract To investigate the impact of different components on the aerodynamic characteristics of hypersonic missiles and missiles’optimization, a numerical simulation model of the typical hypersonic missile aerodynamic optimization was developed based on Ansys/Fluent. Based on this foundation, the missile was three-dimensionally modeled using Solidworks software. Detailed aerodynamic performance analysis was conducted on its head, tail, and canard configuration, which included key aerodynamic performance indicators such as drag coefficient and lift-drag ratio. The research findings indicate th

APA, Harvard, Vancouver, ISO, and other styles

2

Sang, D.-K., and M.-J. Tahk. "Guidance law switching logic considering the seeker's field-of-view limits." Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 223, no. 8 (2009): 1049–58. http://dx.doi.org/10.1243/09544100jaero614.

Full text

Abstract:

The impact time control guidance (ITCG) method, which has been proposed recently, can be applied successfully to a salvo attack of multiple missiles. Compared to the proportional navigation guidance law, this guidance method makes additional manoeuvres to synchronize the impact times. However, such manoeuvres do not consider the manoeuvrability and the seeker's field-of-view (FOV) of a missile and may cause the target to move out of the missile seeker's FOV; maintaining the seeker lock-on condition during the engagement is critical for missile guidance. To solve this problem, two methods are p

APA, Harvard, Vancouver, ISO, and other styles

3

Parshkova, J. Yu. "The Development of the US National Missile Defense and its Impact on the International Security." MGIMO Review of International Relations, no. 1(40) (February 28, 2015): 43–48. http://dx.doi.org/10.24833/2071-8160-2015-1-40-43-48.

Full text

Abstract:

The article reflects the US officials' point of view on the development of its national missile defense. The major threat to international security is the proliferation of ballistic missiles and weapons of mass destruction. The United States and the former Soviet Union made huge efforts to reduce and limit offensive arms. However, presently the proliferation of ballistic missiles spreads all over the world, especially in the Middle East, because of the ballistic missile technology falling into the hands of hostile non-state groups. Missile defenses can provide a permanent presence in a region

APA, Harvard, Vancouver, ISO, and other styles

4

Li, Yang, Hao Zhou, and Wanchun Chen. "Three-Dimensional Impact Time and Angle Control Guidance Based on MPSP." International Journal of Aerospace Engineering 2019 (February 24, 2019): 1–16. http://dx.doi.org/10.1155/2019/5631723.

Full text

Abstract:

A new nonlinear guidance law for air-to-ground missile cooperation attacks is proposed in this paper. This guidance law enables missiles with different initial conditions to attack targets simultaneously, and it can also precisely satisfy the terminal impact angle conditions in both flight-path angle and heading angle. The guidance law is devised using the model predictive static programming (MPSP) method, and the control saturation constraint is incorporated in the MPSP algorithm. The first-order-lag acceleration of the missile is taken as the state variable to realize the convergence of the

APA, Harvard, Vancouver, ISO, and other styles

5

Ghazala Yasmin Jalil. "Missile Race in South Asia: Security Challenges for Pakistan in the 21st Century." Strategic Studies 40, no. 1 (2022): 39–57. http://dx.doi.org/10.53532/ss.040.01.0085.

Full text

Abstract:

The article assesses the nature of missile competition between India and Pakistan and how it impacts deterrence and strategic stability in South Asia. It also analyses how their respective ballistic and cruise missile programmes developed. Taking the action-reaction model of arms racing, it concludes that there is indeed such a dynamic at play between the two countries. The missiles competition is very much linked to the nuclear competition as well. India’s Ballistic Missile Defence (BMD) system also factors into the competitions, whereby Pakistan was forced to develop missiles that could satu

APA, Harvard, Vancouver, ISO, and other styles

6

Li, Quancheng, Tian Yan, Mengjing Gao, Yonghua Fan, and Jie Yan. "Optimal Cooperative Guidance Strategies for Aircraft Defense with Impact Angle Constraints." Aerospace 9, no. 11 (2022): 710. http://dx.doi.org/10.3390/aerospace9110710.

Full text

Abstract:

Given the limitations of escape maneuvers and decoy deployment of combat aircraft under missile attacks; active defense dramatically improves the survival chances by launching active defense missiles to intercept incoming missiles. Different from previous work, this paper implemented impact angle constraints on the defense missile to achieve a better defense effect. The low-cost active defense missile with limited maneuverability is considered to cooperate with the aircraft through three mechanisms, namely two-way cooperation without any predetermined strategy, one-way cooperation with the def

APA, Harvard, Vancouver, ISO, and other styles

7

Wang, Cheng Cheng, Xiao Fang Xie, and Long Jie Zhang. "Vulnerability Analysis of Typical Anti-Ship Missile." Advanced Materials Research 580 (October 2012): 334–37. http://dx.doi.org/10.4028/www.scientific.net/amr.580.334.

Full text

Abstract:

At present the naval gun is the main force of short-range anti-missile. The small caliber naval guns’ impact and penetration effect are the main factors for damaging anti-ship missile. In this paper, the damage mechanism of the anti-ship missile and the vulnerability of a typical missile are studied. On the basis of that, vulnerability function of anti-ship missile is put forward and vulnerability model of one of the important parts of the missile with typical material is built and simulated. It’s useful to the study of the further model of vulnerability analysis of whole anti-ship missiles.

APA, Harvard, Vancouver, ISO, and other styles

8

Feng, Lin Ping, Zuo E. Fan, and You Gen Zhang. "Design of Guidance Law with Impact Angle and Impact Time Constraints." Advanced Materials Research 945-949 (June 2014): 1493–99. http://dx.doi.org/10.4028/www.scientific.net/amr.945-949.1493.

Full text

Abstract:

In order to achieve the tactical mission of cooperative attack for multi-missiles, in a predetermined direction at a predetermined time, this paper studies the design of guidance law with impact angle and impact time constraints. Firstly, using the optimal control theory, the optimal guidance law is designed to control the impact angle, based the relative motion between missile and target. Then the state feedback guidance law is designed to control the arrival impact time, with the application of feedback linearization control theory. Finally, reference the design idea of two-stage guidance sy

APA, Harvard, Vancouver, ISO, and other styles

9

CICHOCKI, Maciej K., Dariusz SOKOŁOWSKI, and Zbigniew LEWANDOWSKI. "Influence of Mass Parameters Modification on Manoeuvrability of 9K33 „OSA” Set 9M33M3 Missile." Problems of Mechatronics Armament Aviation Safety Engineering 11, no. 3 (2020): 9–18. http://dx.doi.org/10.5604/01.3001.0014.3704.

Full text

Abstract:

This paper discusses analytical method for realization of preliminary missile stability design calculations. Action has been taken to estimate influence of replacing massive blocks of analogue electronics with compact solutions of digital electronics in missiles remaining in operation. On an example of a short-range 9M33M3 missile from 9K33 „OSA” set and its previously analysed aerodynamic characteristics, the analysis of the centre of gravity location impact was carried out to determine maximum loads occurring in the two most interesting phases of flight: after booster engine burnout and dire

APA, Harvard, Vancouver, ISO, and other styles

10

Indyk, Jarosław. "The impact of the proliferation of ballistic missiles technology on international security." Polish Political Science Yearbook 52, no. 3 (2023): 165–79. http://dx.doi.org/10.15804/ppsy202384.

Full text

Abstract:

Due to the rapid development of technology after the Second World War, the way of conducting conflict has changed significantly. One of the branches of the armaments industry that has developed the most is space technology and related to it ballistic missiles. Undoubtedly, possession by international entity ballistic missile technology, especially in connection with weapons of mass destruction, increases the importance and role of this entity on the international arena. Therefore, the proliferation of this technology or ready-made missile systems has a significant impact on regional and intern

APA, Harvard, Vancouver, ISO, and other styles

11

Vepsä, Ari, Arja Saarenheimo, Francois Tarallo, Jean-Mathieu Rambach, and Nebojsa Orbovic. "Impact Tests for IRIS_2010 Benchmark Exercise." Journal of Disaster Research 7, no. 5 (2012): 619–28. http://dx.doi.org/10.20965/jdr.2012.p0619.

Full text

Abstract:

IRIS_2010 benchmark was an exercise in OECD/NEA/CSNI framework. This exercise concentrated on improving robustness assessment methodologies for structures impacted by missiles. This article describes experimental tests included in the exercise. These tests consisted of two tests for bending, three for punching and one for combined punching and bending behaviour of reinforced concrete walls under impact loading. The test for combined behaviour was carried out in Meppen, Germany in the 1980’s, while all the other tests were carried out by VTT Technical research centre of Finland during the sprin

APA, Harvard, Vancouver, ISO, and other styles

12

Pravidlo, M. N., A. Y. Korolev, and L. V. Bykov. "Investigation into the dependence of ballistic characteristics of rockets on atmospheric parameters." Journal of «Almaz – Antey» Air and Space Defence Corporation, no. 3 (September 30, 2018): 37–47. http://dx.doi.org/10.38013/2542-0542-2018-3-37-47.

Full text

Abstract:

When calculating the ballistic characteristics of a tactical missile, the atmospheric parameters have a significant impact on determining possible launch and missile engagement zones. The paper introduces the results of comparing the standard atmospheric parameters according to the State Standard GOST 4401-81 “Standard atmosphere. Parameters” and four empirical models of the atmosphere obtained from radio sounding data in different climatic zones and at different times of the year. By the example of a hypothetical air-to-air missile, we demonstrate possible launch and missile engagement zones

APA, Harvard, Vancouver, ISO, and other styles

13

Toshev, O. T., O. M. Maksymov, and M. V. Kiriakidi. "SIMULATION MODEL OF A MISSILE STRIKE." ELECTRICAL AND COMPUTER SYSTEMS, no. 40(116) (2024): 63–76. http://dx.doi.org/10.15276/eltecs.40.116.2024.7.

Full text

Abstract:

Abstract. As modern naval warfare systems and tactics continue to evolve, it is crucial to employ contemporary tools capable of assessing their potential across various combat scenarios. This study model simulates interactions between anti-ship missiles and naval forces during landing operations. Our research seeks to develop a robust method for quantitatively analyzing the impact of anti-ship missiles on naval vessels under diverse combat conditions. The model's scalability allows for the incorporation of emerging naval tactics and procedures, maintaining its relevance and utility in dynamic

APA, Harvard, Vancouver, ISO, and other styles

14

Krivolapov, Oleg O. "Regional Missile Defense Architecture of the US and Their Partners In the Western Pacifi Security." Obshchestvennye nauki i sovremennost, no. 3 (December 15, 2023): 39–53. http://dx.doi.org/10.31857/s0869049923030036.

Full text

Abstract:

China has the largest arsenal of missiles with a range of less than 5,500 km. In 2019, the US withdrew from the INF Treaty and decided to deploy the same kind of missiles in East Asia. At the same time Washington plans to strengthen the theater missile defense architecture in the region. The purpose of the article is to determine the potential impact of missile defense strengthening by the US and their partners in East Asia on regional security. It is necessary to understand the prospects of the situation, given the presence of several hotbeds of potential conflict in the Western Pacific. A cr

APA, Harvard, Vancouver, ISO, and other styles

15

Krivolapov, O. O. "The Influence of NATO Regional Missile Defense on European Security." Herald of the Russian Academy of Sciences 92, S4 (2022): S301—S307. http://dx.doi.org/10.1134/s1019331622100100.

Full text

Abstract:

Abstract The problem of missile defense is considered by Russian researchers, first of all, as part of the strategic stability problem in relations between Russia and the United States. At the same time, the impact of regional missile defense (theater missile defense) on regional security remains largely unexplored. The US and NATO leadership continue to claim that Russia has deployed intermediate-range missiles in the European part of the country. As a response to this step, in addition to other measures of regional deterrence towards Russia, it is planned to strengthen NATO’s regional missil

APA, Harvard, Vancouver, ISO, and other styles

16

SULISTYAWATI, Laeny, and Peni HANGGARINI. "Iran's Hypersonic Missile Attack on Israel and Its Impact on Geopolitics and Oil Prices." Journal of Political And Legal Sovereignty 2, no. 1 (2024): 200–210. https://doi.org/10.38142/jpls.v2i1.211.

Full text

Abstract:

Purpose:This paper explores Iran's missile attacks on Israel in April 2024 and October 2024 that have had an impact on the Middle East. On October 1, 2024, more than 180 ballistic missiles were fired into the skies of Israel. Iran officially admitted firing hypersonic missiles into Israel in retaliation for Israel's campaign against Iran's ally Hezbollah in Lebanon.Methodology:The research method used in this paper is qualitative descriptive-analytical. Qualitative method: Data is collected from literature studies in the form of books, articles, news, internet-based studies, digital books, pre

APA, Harvard, Vancouver, ISO, and other styles

17

Abbas, H., D. K. Paul, P. N. Godbole, and G. C. Nayak. "Soft missile impact on rigid targets." International Journal of Impact Engineering 16, no. 5-6 (1995): 727–37. http://dx.doi.org/10.1016/0734-743x(95)00004-t.

Full text

APA, Harvard, Vancouver, ISO, and other styles

18

Pande, Savita. "Missile technology control regime: Impact assessment." Strategic Analysis 23, no. 6 (1999): 923–45. http://dx.doi.org/10.1080/09700169908455096.

Full text

APA, Harvard, Vancouver, ISO, and other styles

19

Zhang, Ziqi, Zhongjie Yin, Wanli Meng, Zhengyu Lu, and Tianwei Song. "Sliding mode guidance law with Field-of-view constraint and impact time control for missiles." Journal of Physics: Conference Series 2955, no. 1 (2025): 012029. https://doi.org/10.1088/1742-6596/2955/1/012029.

Full text

Abstract:

Abstract This study introduces an innovative guidance law that allows for controlled impact time while meeting the missile’s field-of-view angle constraints. The equation that shows the missile-target relative movement is first established. A non-singular sliding mode guidance law is designed, leveraging sliding mode control theory. Under the field-of-view constraints, the impact time reaches the desired value, as proven according to the Lyapunov stability theory. The analyses derived from the numerical simulation support that the missile’s field-of-view angle remains within constraints throug

APA, Harvard, Vancouver, ISO, and other styles

20

Pietraszek, Mariusz, and Tomasz Klemba. "Investigation of the Oxidizer Charge Impact Onto Energetic Characteristics Demonstrated by the Stream of Gunpowder Gas Ejected by Solid-Propellant Missile Engines." Research Works of Air Force Institute of Technology 33, no. 1 (2013): 203–19. http://dx.doi.org/10.2478/afit-2013-0012.

Full text

Abstract:

Abstract The study discloses outputs from examinations devoted to charges of oxidizers and their impact on behaviour of missile engine operation with particular attention to measures that are undertaken to counteract stall of a helicopter engine. Homogenous solid propellant for missile engines exhibits a negative oxygen balance. When a series of rocket missiles driven by means of such fuel is launched from the helicopter board there is a hazard of the engine stall effect that may lead to killing its engines. Admixture of potassium (II) sulphate (VI) that is added into the combustion chamber of

APA, Harvard, Vancouver, ISO, and other styles

21

Pinchuk, A., M. Garbuz, P. Zeleny, D. Harnets, and D. Ivanov. "ANALYSIS OF EXPERIENCE IN THE APPLICATION OF MISSILE LAUNCH DETECTION SYSTEMS." Наукові праці Державного науково-дослідного інституту випробувань і сертифікації озброєння та військової техніки, no. 9 (December 3, 2021): 118–29. http://dx.doi.org/10.37701/dndivsovt.9.2021.14.

Full text

Abstract:

Analysis of combat losses of aircraft in local armed conflicts in recent decades shows that most cases of aircraft hits are related to the impact of guided surface-to-air and air-to-air missiles equipped with homing warheads. The use of modern guided missiles equipped with homing warheads is one of the main threats to aircraft of various types. This is due to the fact that modern guided missiles are characterized by high speed, maneuverability, accuracy of aiming and difficulty of detection. Solving the problem of protecting aircraft from guided missiles consists of several stages:

APA, Harvard, Vancouver, ISO, and other styles

22

Maruyama, Takashi, Hiromasa Kawai, Hiroaki Nishimura, and Mayuko Hanatani. "Missile Impact Resistant Test of Glasses According to ISO 16932." Journal of Disaster Research 8, no. 6 (2013): 1114–19. http://dx.doi.org/10.20965/jdr.2013.p1114.

Full text

Abstract:

The importance of protecting windows from windborne debris has been pointed out in many reports on wind induced disaster. In Japan, there are still no building codes or standards to protect cladding from wind-borne debris. In contrast, both American and ISO standards cover specifications, including testing methods, for cladding performance under impact by wind-borne debris. A series of impact tests was conducted to evaluate the safety of different types of window glasses. This paper describes results for impact resistant tests, including destruction modes, for float glass, tempered glass, wire

APA, Harvard, Vancouver, ISO, and other styles

23

Dziopa, Z., and Z. Koruba. "The impact of launcher turret vibrations control on the rocket launch." Bulletin of the Polish Academy of Sciences Technical Sciences 63, no. 3 (2015): 717–28. http://dx.doi.org/10.1515/bpasts-2015-0083.

Full text

Abstract:

Abstract The paper discusses the missile lift-off from a launcher placed on a motor vehicle. The stimulation of the assembly vibration results from the input generated by the road and the missile firing. The unfavourable input generated in the course of assembly operation has an impact on the characteristics of the initial missile flight parameters. The aim of the paper is to apply the hybrid vibroisolation system of the launcher turret in order to improve the conditions of the missile launch from the assembly. The active system reducing the occurring disturbance allows to control the launcher

APA, Harvard, Vancouver, ISO, and other styles

24

Shetty, Mahesh S., Lokeswarappa R. Dharani, and Daniel S. Stutts. "Analysis of Laminated Architectural Glazing Subjected to Wind Load and Windborne Debris Impact." ISRN Civil Engineering 2012 (September 2, 2012): 1–9. http://dx.doi.org/10.5402/2012/949070.

Full text

Abstract:

During windstorms and hurricanes, architectural glazing is subjected to wind loading and windborne debris impact. Wind-borne debris is categorized into two types. One is small hard missile like roof gravel and the other is large soft missile representing the lumber from wood-framed buildings. Laminated architectural glazing (LAG) is the commonly used glazing in buildings where impact resistance is needed. The prefailure stress response of the LAG due to the combined loading due to wind and windborne debris impact is studied. Following the ASTM standards (E1886 and E1996), a steel ball with an

APA, Harvard, Vancouver, ISO, and other styles

25

Tuomala, Markku, Kim Calonius, Arja Saarenheimo, and Pekka Välikangas. "Hard Missile Impact on Prestressed Shear Reinforced Slab." Journal of Disaster Research 5, no. 4 (2010): 437–51. http://dx.doi.org/10.20965/jdr.2010.p0437.

Full text

Abstract:

The protective concrete walls of nuclear power plants must withstand accidental or intentional missile impact, and structural systems and solutions are being developed in building frameworks and detailed levels requiring sophisticated tools for different design phases such as detailing shear reinforcement. Numerical methods, for example, have been developed and used for predicting prestressed shear reinforced concrete structures response subjected to hard projectile impact. The structural behavior of prestressed impact-loaded walls is predicted analytically and by using nonlinear FE models. An

APA, Harvard, Vancouver, ISO, and other styles

26

Krivolapov, O. O. "Missile Defense of the U.S. and Their Allies in Northeast Asia and Regional Security." Asia and Africa today, no. 6 (December 15, 2024): 5–14. http://dx.doi.org/10.31857/s032150750031033-8.

Full text

Abstract:

The situation around the Korean Peninsula combines such factors as nuclear weapons, missile defense systems, and huge groups of conventional armed forces concentrated in Northeast Asia. The U.S. administration argues that missile defense’s mission is to counter the threat from North Korean missiles to American and allied troops in South Korea and Japan. Hence, this line of confrontation between the U.S. and DPRK is at the focus of the article. A significant number of experts believe that regional missile defense (theater missile defense, TMD) will only stabilize the situation. The purpose of t

APA, Harvard, Vancouver, ISO, and other styles

27

Hou, Libing, Jihong Zhu, Minchi Kuang, and Heng Shi. "Impact Angle Control Guidance to Intercept Moving Targets by Virtual Target Technique." International Journal of Aerospace Engineering 2021 (December 21, 2021): 1–12. http://dx.doi.org/10.1155/2021/7210808.

Full text

Abstract:

To solve the problem regarding the impact angle of the missile, this paper proposes a novel guidance law, which can control the missile to hit the target at the desired angle. The key of the guidance law is selecting a moving point on the collision line as the virtual target, and the tactical requirements can be fulfilled by the missile directly pursuing the virtual target. The Lyapunov stable theory is used to prove the convergence of the proposed guidance law. The guidance command is generated by a PID controller to make the missile towards the virtual target. The proposed guidance law makes

APA, Harvard, Vancouver, ISO, and other styles

28

Yazdani, PhD, Nur, Perry Green, PhD, and Saif Haroon, PhD. "Wind-missile impact capacity of essential facilities." Journal of Emergency Management 5, no. 2 (2007): 27. http://dx.doi.org/10.5055/jem.2007.0053.

Full text

Abstract:

Windborne debris during a hurricane may cause damage to building façades, resulting in significant economic losses and injury or death. Recent building codes have adopted variations of the large-wind-missile impact test in order to certify roof/wall components for hurricane resistance. The purpose of this study was to investigate the performance of commonly used Florida wall and roof assemblies under enhanced large-wind-missile impact testing, beyond the basic test specified in the Florida Building Code. Relevant standards specify similar enhanced standards for essential facilities and shelter

APA, Harvard, Vancouver, ISO, and other styles

29

Vardanega, C., M. G. Cremonini, M. Mirone, and A. Luciani. "Response of buried pipes to missile impact." Nuclear Engineering and Design 115, no. 1 (1989): 91–103. http://dx.doi.org/10.1016/0029-5493(89)90262-8.

Full text

APA, Harvard, Vancouver, ISO, and other styles

30

Yang, Yanhong, Rosa Lo Frano, Hao Wu, and Salvatore Cancemi. "ANALYSIS OF SLAB PERFORATION UNDER MISSILE IMPACT." Proceedings of the International Conference on Nuclear Engineering (ICONE) 2023.30 (2023): 1265. http://dx.doi.org/10.1299/jsmeicone.2023.30.1265.

Full text

APA, Harvard, Vancouver, ISO, and other styles

31

MARUYAMA, Takashi, Hiromasa KAWAI, Hiroaki NISHIMURA, and Mayuko HANATANI. "Missile Impact Resistant Test for Laminated Glasses using Various Missiles and a Proposal of Standard Missiles." Journal of Wind Engineering 39, no. 1 (2014): 1–12. http://dx.doi.org/10.5359/jwe.39.1.

Full text

APA, Harvard, Vancouver, ISO, and other styles

32

Wang, Wei Jie, Huai Rong Shen, and Yi Yong Li. "Study on the Kinetic Anti-Missile Fragment Based on NASA Model." Applied Mechanics and Materials 271-272 (December 2012): 584–88. http://dx.doi.org/10.4028/www.scientific.net/amm.271-272.584.

Full text

Abstract:

The question of the anti-missile fragment produced by the Kinetic Kill Vehicle (KKV) intercepting the Tactical Ballistic Missile (TBM) is studied. It turns out the anti-missile fragment are composite outcome of the impact and explosion. By analysis the National Aeronautics and Space Administration (NASA) impact breakup model is suggested to calculate the fragment charac-teristic. The minimum mass threshold of effective fragment is deduced; the damages probability model that the debris cloud impacts the cooperative target is established based on Poisson distribu-tion. The simulation case indica

APA, Harvard, Vancouver, ISO, and other styles

33

Cong, Mingyu, Xianghong Cheng, Zhiquan Zhao, and Zhijun Li. "Studies on Multi-Constraints Cooperative Guidance Method Based on Distributed MPC for Multi-Missiles." Applied Sciences 11, no. 22 (2021): 10857. http://dx.doi.org/10.3390/app112210857.

Full text

Abstract:

Cooperative terminal guidance with impact angle constraint is a key technology to achieve a saturation attack and improve combat effectiveness. The present study envisaged cooperative terminal guidance with impact angle constraint for multiple missiles. In this pursuit, initially, the three-dimensional cooperative terminal guidance law with multiple constraints was studied. The impact time cooperative strategy of virtual leader missile and follower missiles was designed by introducing virtual leader missiles. Subsequently, based on the distributed model prediction control combined with the par

APA, Harvard, Vancouver, ISO, and other styles

34

Toshev, Oleksandr, Oleksii Maksymov, Maksym Kiriakidi, and Maksym Maksymov. "Missile Strike Simulation in a Video Game Engine." Energy engineering and control systems 10, no. 1 (2024): 43–55. http://dx.doi.org/10.23939/jeecs2024.01.043.

Full text

Abstract:

In the field of modern computer gaming (especially within the genre of war-game strategies, realistic first-person shooters and other warfare games) the complexity of virtual naval warfare mechanics and strategies significantly increases. There is a growing demand for advanced simulation tools to provide more immersive experience and more complex gameplay for all players. The goal of this research is to create a model and tool that can accurately predict the impact of anti-ship missiles on ships engaged in different game scenarios, considering a wide range of battle conditions. By encompassing

APA, Harvard, Vancouver, ISO, and other styles

35

Yunda, Valerii, Vladislav Mizin, and Maksym Vyhovskyi. "Analysis of the enemy's electronic warfare and air defense capabilities regarding their impact on the effectiveness of strikes on targets by M142 “HIMARS” and M270 “MLRS” missile systems." Military Technical Collection, no. 31 (December 17, 2024): 57–64. https://doi.org/10.33577/2312-4458.31.2024.57-64.

Full text

Abstract:

The article analyzes the capabilities of the electronic warfare and air defense systems of the Armed Forces of the russian federation, which conducted fire strikes and electronic suppression of precision-guided missiles of the “GMLRS” and “ATACMS“ families, affecting the effectiveness of strikes on targets by missile units of the Armed Forces of Ukraine, equipped with M142 “HIMARS” and M270 “MLRS” missile systems. The experience gained by leading countries in local conflicts has demonstrated the crucial importance of this type of weaponry. However, in most cases, the opposing forces in these l

APA, Harvard, Vancouver, ISO, and other styles

36

Zhou, Jun, Yang Wang, and Bin Zhao. "Impact-Time-Control Guidance Law for Missile with Time-Varying Velocity." Mathematical Problems in Engineering 2016 (2016): 1–14. http://dx.doi.org/10.1155/2016/7951923.

Full text

Abstract:

The problem of impact-time-control guidance (ITCG) for the homing missile with time-varying velocity is addressed. First, a novel ITCG law is proposed based on the integral sliding mode control (ISMC) method. Then, a salvo attack algorithm is designed based on the proposed guidance law. The performances of the conventional ITCG laws strongly depend on the accuracy of the estimated time-to-go (TTG). However, the accurate estimated TTG can be obtained only if the missile velocity is constant. The conventional ITCG laws were designed under the assumption that the missile velocity is constant. The

APA, Harvard, Vancouver, ISO, and other styles

37

Gao, C., J. Li, T. Feng, and W. Jing. "Adaptive terminal guidance law with impact-angle constraint." Aeronautical Journal 122, no. 1249 (2017): 369–89. http://dx.doi.org/10.1017/aer.2017.124.

Full text

Abstract:

ABSTRACTThis paper proposes an adaptive guidance law for attacking a ground target based on motion camouflage strategy. The coefficients of normal and bi-normal feedback guidance law are given according to the relative motion relationship under Frenet frame. Utilizing the coefficients, the motion camouflage proportional guidance law is derived. In order to improve the initial overload characteristic of the missile, an adaptive feedback coefficient is introduced. Then, the adaptive guidance law is applied to a longitudinal plane interception problem with impact-angle constraint. Finally, the va

APA, Harvard, Vancouver, ISO, and other styles

38

Wang, Jian Hua, Yuan Wen Cai, Long Cheng, et al. "Active disturbance rejection guidance and control scheme for homing missiles with impact angle constraints." Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 233, no. 3 (2018): 1133–46. http://dx.doi.org/10.1177/0954410017748968.

Full text

Abstract:

An active disturbance rejection guidance and control scheme for homing missiles with three-dimensional impact angle constraints is proposed. The six-degree-of-freedom dynamical and kinematical models containing model uncertainties and disturbances are established. A strict feedback relative dynamics between the target and homing missile in three-dimensional space are deduced. A reconstructed reduced-order attitude controller design model is proposed. A two-loop control structure with respect to the centroid guidance loop and rotational control loop is conducted to implement the six-degree-of-f

APA, Harvard, Vancouver, ISO, and other styles

39

Adler, Jacov. "Medical and Surgical Issues in the Persian Gulf War." Prehospital and Disaster Medicine 12, no. 1 (1997): 73–76. http://dx.doi.org/10.1017/s1049023x00037262.

Full text

Abstract:

AbstractThis report includes the preparations for and the medical impact of the missile attacks launched by Iraq on Israel. It includes the authorization language for the preparations, the preparations undertaken, the perceived threat to the civilian population of Israel, the operational plans activated, the attacks and the medical impact of these attacks, the number and types of casualties, the damage to property, and the initial and subsequent protection times. There occurred a total of 18 missile attacks with 40 conventional missiles launched against Israeli civilians. They resulted in an 4

APA, Harvard, Vancouver, ISO, and other styles

40

Shang, Wei, Jie Guo, Shengjing Tang, Yueyue Ma, and Yao Zhang. "Impact Time Guidance Law Considering Autopilot Dynamics Based on Variable Coefficients Strategy for Maneuvering Target." Mathematical Problems in Engineering 2015 (2015): 1–10. http://dx.doi.org/10.1155/2015/815149.

Full text

Abstract:

This paper investigates the terminal guidance problem for the missile intercepting a maneuvering target with impact time constraint. An impact time guidance law based on finite time convergence control theory is developed regarding the target motion as an unknown disturbance. To further improve the performance of the guidance law, an autopilot dynamics which is considered as a first-order lag is taken into consideration. In the proposed method, the coefficients change with the relative distance between missile and target. This variable coefficient strategy ensures that the missile impacts the

APA, Harvard, Vancouver, ISO, and other styles

41

Lulec, Andac, and Frank J. Vecchio. "A Simplified Approach to Analysis of Reinforced Concrete Slabs Subjected to Hard Missile Impacts." Key Engineering Materials 711 (September 2016): 924–31. http://dx.doi.org/10.4028/www.scientific.net/kem.711.924.

Full text

Abstract:

This paper presents a nonlinear finite element analysis (NLFEA) procedure employing a smeared rotating crack macro-modeling approach for analysis of reinforced concrete structures under hard missile impacts. It represents a middle ground between simplified methods based on single degree of freedom (SDOF) systems and complex meso-or micro-element hydrocodes. Three hard missile impact tests were modeled and the results were compared with experimental results in terms of residual velocity, damage shape, and impact depth. Good correlations were obtained.

APA, Harvard, Vancouver, ISO, and other styles

42

Siddiqui, N. A. "A Simplified Procedure for Reliability Estimation of Underground Concrete Barriers against Normal Missile Impact." Journal of Engineering Research [TJER] 7, no. 2 (2011): 61. http://dx.doi.org/10.24200/tjer.vol8iss1pp61-73.

Full text

Abstract:

Underground concrete barriers are frequently used to protect strategic structures like Nuclear power plants (NPP), deep under the soil against any possible high velocity missile impact. For a given range and type of missile (or projectile) it is of paramount importance to examine the reliability of underground concrete barriers under expected uncertainties involved in the missile, concrete, and soil parameters. In this paper, a simple procedure for the reliability assessment of underground concrete barriers against normal missile impact has been presented using the First Order Reliability Meth

APA, Harvard, Vancouver, ISO, and other styles

43

Károlyi, György, and András Á. Sipos. "Soft impact of an elongated elasto-plastic missile." International Journal of Mechanical Sciences 212 (December 2021): 106804. http://dx.doi.org/10.1016/j.ijmecsci.2021.106804.

Full text

APA, Harvard, Vancouver, ISO, and other styles

44

Saarenheimo, Arja, Kim Calonius, Markku Tuomala, and Ilkka Hakola. "Soft Missile Impact on Shear Reinforced Concrete Wall." Journal of Disaster Research 5, no. 4 (2010): 426–36. http://dx.doi.org/10.20965/jdr.2010.p0426.

Full text

Abstract:

In developing numerical approaches for predicting the response of reinforced concrete structures impacted on by deformable projectiles, we predict structural behavior collapse and damage using simple analysis and extensive nonlinear finite element (FE)models. To verify their accuracy, we compared numerical results to experimental data and observations on impact-loaded concrete walls with bending and transverse shear reinforcement. Different models prove adequate for different cases and are sensitive to different variables, making it important to rely on more than a single model alone. For wall

APA, Harvard, Vancouver, ISO, and other styles

45

Markham, K. C. "IMPACT: A computer program to aid missile system design." Aeronautical Journal 94, no. 931 (1990): 24–35. http://dx.doi.org/10.1017/s000192400002234x.

Full text

Abstract:

The design of guided missile systems presents a wide spectrum of problems to engineers in numerous disciplines which range through aerodynamics, electronics and signal processing. Of all the tasks involved in the design process, perhaps the most difficult is the integration of the various technologies into a complete, harmonised system. IMPACT is a computer program which was developed to address the system design aspects of homing guidance missile systems. The aim of this paper is to describe the engineering philosophy and theoretical background to the IMPACT program.

APA, Harvard, Vancouver, ISO, and other styles

46

Shang, Shu Cong, and Jian Zhong Sun. "Research on the Affection of the Underwater Missile Launching Process." Applied Mechanics and Materials 130-134 (October 2011): 2594–99. http://dx.doi.org/10.4028/www.scientific.net/amm.130-134.2594.

Full text

Abstract:

A dynamic model and numerical method which was in the underwater vertical launching process have been built, and the missile which was on the effects of the lateral flow was simulated with its movement and load. The results showed that: the model is feasible; adapter compressive stiffness and its layout in the tube has a greater impact on the movement and load of the missile; fluid added mass effect is not negligible; the lateral movement of the missile’s launching process was along with a large shock , so we must attach importance to the problem of vibration. lateral flow

APA, Harvard, Vancouver, ISO, and other styles

47

Han, Yu Long, Jian Gang Yan, Yun Lin, Qian Yu Zhang, and Qi Shuang Huo. "Air Ship Missile Carrier Aircraft Attack Array Model Research." Applied Mechanics and Materials 687-691 (November 2014): 1436–42. http://dx.doi.org/10.4028/www.scientific.net/amm.687-691.1436.

Full text

Abstract:

This paper studies air defense system kill zone, air ship missile firing mode and air ship missile launch area that impact air ship missile load matrix determine key problems, establishes air ship missile carrier array’s mathematics model, makes simulation calculation of the model, and analyzes simulation results, and gets the influence law of vehicle speed, height, target motion characteristics, deviation angle and pitching angle on attack matrix, and the results can provide reference for determining air ship missile carrier aircraft attack array.

APA, Harvard, Vancouver, ISO, and other styles

48

Brown, Samuel J. "Energy Release Protection for Pressurized Systems. Part II: Review of Studies Into Impact/Terminal Ballistics." Applied Mechanics Reviews 39, no. 2 (1986): 177–201. http://dx.doi.org/10.1115/1.3143704.

Full text

Abstract:

In order to assess whether or not there is a need for protection against the failure of a pressure system, the engineer must evaluate the hazards associated with rupture. The hazards are divided into two categories: (a) force/displacement and (b) degenerative. Force/displacement is classified into (1) kinetic energy associated with the atmosphere: blast, (2) kinetic energy of objects (fragmentation and impact of missiles), and (3) kinetic energy associated with foundations: soil foundation motion. The first article of this series [Energy release protection from pressurized systems: Part I Revi

APA, Harvard, Vancouver, ISO, and other styles

49

WANG, Zhuo, Tao WANG, Bo ZHANG, and Hong-wen MA. "Analysis and Experimental Research on Test Method of Initial Guidance Thrust." Mechanics 26, no. 5 (2020): 398–406. http://dx.doi.org/10.5755/j01.mech.26.5.23460.

Full text

Abstract:

With the gradual development of aerospace industry, the demand for missile performance is also growing. The steering gear, as one of the main implementing agencies of the missile guidance and control system, can adjust the actual thrust size through the closed-loop control system during missile guidance the deflection angle of the rudder surface, in order to change the missile's flight speed and flight attitude. The missile during the flight attitude correction and speed adjustment are through the electric servo output power to change the size of the output to complete. In this paper, the unst

APA, Harvard, Vancouver, ISO, and other styles

50

Lim, Chin Beng, and Muataz H. Salih. "Design and implementation of embedded concurrent laser missile jammer system using FPGA." Indonesian Journal of Electrical Engineering and Computer Science 14, no. 2 (2019): 780. http://dx.doi.org/10.11591/ijeecs.v14.i2.pp780-787.

Full text

Abstract:

<span>In real time system, every second takes into count as any extra delay could cause critical consequences. Nowadays, almost every system involving multiple data processing. To handle multiple data at the same time, spatial parallelism is required to enhance system performance and provide multitasking feature. Currently, frequency jamming system only can jam one signal at a time. When it comes to missile jamming, the delaying in processing the frequency could cause serious impact as there will be multiple missiles launched to hit a target. These missiles just need few seconds to hit t

APA, Harvard, Vancouver, ISO, and other styles

We offer discounts on all premium plans for authors whose works are included in thematic literature selections. Contact us to get a unique promo code!