• Title/Summary/Keyword: Air-to-Air Combat

Search Result 137, Processing Time 0.021 seconds

Pursuit-evasion as a dynamic game

  • Imado, Fumiaki;Ichikawa, Akira;Kanai, Kimio
    • 제어로봇시스템학회:학술대회논문집
    • /
    • 1993.10b
    • /
    • pp.474-479
    • /
    • 1993
  • A study about two-dimensional pursuit-evasion dynamic games is presented and discussed. A pursuer tries to intercept an evader by a strategy based on proportional navigation guidance, while the evader tries to maximize a miss distance by the optimal control. The study is applied to a ball game and an air-combat game. The results show the same features exist in both games, therefore the study will be able to apply for general two dimensional dynamic games. In the ball game, the study is extended to cases where a goal exists, while in the air-combat game, some three-dimensional problems are solved and the results are also shown.

  • PDF

Following the Cold War, both the United States' military operational concept and the Republic of Korea Army's developmental study (탈냉전기 미국의 군사작전 개념과 한국군 발전방향 연구-합동작전을 중심으로)

  • Lee, Se-Han
    • Journal of National Security and Military Science
    • /
    • s.2
    • /
    • pp.121-163
    • /
    • 2004
  • Science technique development expanded into, not only land, sea, and air operations but also those of airspace, and cyber battle spaces. It is generally accepted at this time that space centric operations currently cannot be effectively divided from air operations. However, science and technology advancements make it possible to integrate Army, Navy, Airforce, and Marine forces into effective operations as never before. The Republic of Korea Armed Forces needs to establish a more effective joint concept. The US military, considered by many experts as the most effective in the world, understands the necessity of joint operations and accordingly has highly developed its own concept of joint operations. The US joint operational concepts demonstrated their effectiveness during the Iraqi War by dominating the battlefield through effective use of all combat and non-combat power. Following the US Iraqi War experience, the US Department of Defense continued to enhance Joint Capability through the acceleration of US Military Transformation involving all components. The future national security of the Republic of Korea, faced with the peculiarity of communist threat in the form of North Korea, and the conflicting interest of four strong powers; the United States, China, Japan, and Russia, depends on small but strong armed forces employing all available combat power through effective National and Military Strategy, and considering domestic and international constraints. In order to succeed in future wars, military operations following joint operational concepts must effectively employ all available combat power in a timely manner. The Republic of Korea Armed Forces must establish a joint forces concept in order to integrate all available combat power during employment. Therefore we must establish military operations that develop the military structure and organization, doctrine, weapon systems, training and education of our armed forces based on the key concept of joint operations.

  • PDF

Development of Simulator for Generating BVR Air Combat Engagement Geometry (BVR 공중전 교전 기하 생성을 위한 시뮬레이터 개발)

  • Juho Choi;IL-Chul Moon;Youngho Kim;Taesub Yun
    • Journal of the Korea Society for Simulation
    • /
    • v.33 no.3
    • /
    • pp.51-63
    • /
    • 2024
  • This study aims to develop a simulator for modeling engagements between fighters and missiles in Beyond Visual Range (BVR) air combat scenarios using DEVS (Discrete Event System specification) formalism. The simulator is modeled to implement sustained formation strategies in 1-versus-many situations, and we applied the model to real scenario two case studies. The two case studies assume a virtual missile neutralization equipment. The first case study analyzes the effectiveness of the missile neutralization equipment based on formations. The second case study analyzes the effectiveness of the missile neutralization equipment in relation to the evasion maneuvering tactic of the formation leader fighter. Through these studies, it is demonstrated that the model can realistically simulate scenarios and be beneficial the development of evasion strategies and tactics.

The Future of Aerospace Weapon Systems based on Aerospace Technology Modeling (항공우주력 기술 모델링에 기반한 미래 항공우주 무기체계 발전방향)

  • Cho, Taehwan;Choi, Insoo;Lee, Soungsub
    • Journal of Advanced Navigation Technology
    • /
    • v.24 no.5
    • /
    • pp.368-373
    • /
    • 2020
  • In order to systematically apply major technologies of the 4th Industrial Revolution to aerospace power development, an aerospace technology model is needed. The Propeller Model, which is an existing aerospace model, is a concept that operates a combination of altitude, speed, and distance, which are basic characteristics of aerospace. However, in the era of the 4th Industrial Revolution, a new model is needed because numerous technologies are used in convergence. In this paper, a jet engine model is proposed as a new aerospace technology model. Also, we propose a procedure for creating future aerospace weapon systems based on aerospace technology modeling, not on operational capability. The utilization of future battlefields and the study of the concept of advanced weapon systems in developed countries can create a new concept of weapon systems.

Techniques study of IMS/SIP based Lawful Interception in 3G networks (3G 네트워크에서의 IMS/SIP 기반 합법적 감청 기법)

  • Lee, Myoung-rak;Pyo, Sang-Ho;In, Hoh Peter
    • Journal of the Korea Institute of Information Security & Cryptology
    • /
    • v.25 no.6
    • /
    • pp.1411-1420
    • /
    • 2015
  • Lawful interception(LI) standard of telephone networks has technical limitations to lawfully intercept IMS/SIP-based mobile communication network subscriber who using Android and iPhone device. In addition, the technical standards related to legal interception of the IMS/SIP of the wireless network is insufficient compared to the systematic study of the development of a wireless network infrastructure. The architecture proposed in the standard of ETSI(European Telecommunications Standards Institute) for the seamless LI is insufficient to overcome the limitations of traditional voice-centric LI techniques. This paper proposes an IMS/SIP-based architecture to perform LI under 3G networks that focuses on mobility-supported environments with merging cellular networks and the Internet. We implemented the simulation to verify the efficiency of the proposed architecture, and the experimental results show that our method achieves higher lawful interception rate than that of existing interception methods.

Numerical Analysis Approach to Calculate the Damage Degree of the Combat Vehicle (전투차량의 피해 정도를 계산하기 위한 수치해석적 접근법)

  • Cho, A Hyoun;Park, Kang;Kim, Gun In
    • Korean Journal of Computational Design and Engineering
    • /
    • v.22 no.2
    • /
    • pp.101-109
    • /
    • 2017
  • In order to reduce the number of casualties by improving the survivability of the combat vehicle, the vulnerability analysis of the combat vehicle is needed. However, the actual test for the vulnerability analysis requires large experimental space and expensive equipment costs long time and large expense. It is needed to develop a new method that can replace the actual test. In the paper, we suggested a new approach to analyzing the vulnerability using the M&S method instead of the actual test. To analyze the vulnerability, the shot line analysis is performed to find out which part is penetrated by the bullet. The component of the parts is simplified to "Single-Target", "Double-Target", "Air gapped-Target" and can be performed the penetration analysis using the ANSYS Explicit Dynamics. The penetration depth and the residual velocity of the bullet are calculated by analyzing penetration of each part of the combat vehicle. The penetration data calculated the penetration analysis can be used to define the damage level of the combat vehicle. The purpose of this paper is to collect penetration data for various targets and bullets. And "7.62mmAP" is used as the bullet, "7075-T6" is used as a target.

Air-Launched Weapon Engagement Zone Development Utilizing SCG (Scaled Conjugate Gradient) Algorithm

  • Hansang JO;Rho Shin MYONG
    • Korean Journal of Artificial Intelligence
    • /
    • v.12 no.2
    • /
    • pp.17-23
    • /
    • 2024
  • Various methods have been developed to predict the flight path of an air-launched weapon to intercept a fast-moving target in the air. However, it is also getting more challenging to predict the optimal firing zone and provide it to a pilot in real-time during engagements for advanced weapons having new complicated guidance and thrust control. In this study, a method is proposed to develop an optimized weapon engagement zone by the SCG (Scaled Conjugate Gradient) algorithm to achieve both accurate and fast estimates and provide an optimized launch display to a pilot during combat engagement. SCG algorithm is fully automated, includes no critical user-dependent parameters, and avoids an exhaustive search used repeatedly to determine the appropriate stage and size of machine learning. Compared with real data, this study showed that the development of a machine learning-based weapon aiming algorithm can provide proper output for optimum weapon launch zones that can be used for operational fighters. This study also established a process to develop one of the critical aircraft-weapon integration software, which can be commonly used for aircraft integration of air-launched weapons.

A Design of Anti-Aircraft Artillery Model for the Surface-to-Air Virtual Engagement (지대공 교전모의를 위한 대공포 모델 설계)

  • Yang, Chang-Deok;Yang, Ji-Youn;Kim, Cheon-Young;Hong, Young-Seok;Reu, Tae-Kyu
    • Journal of the Korea Institute of Military Science and Technology
    • /
    • v.14 no.4
    • /
    • pp.639-647
    • /
    • 2011
  • In this paper, we have designed the Anti-Aircraft Artillery(AAA) model for the surface-to-air virtual engagement. The AAA model for the virtual combat simulation needs to detect the present target and estimate the target flight trajectory to find the aiming point. To find collision point of projectile fired from the artillery with the moving air target, we have presented the estimating technique for artillery aiming point. And we have analyzed the target probability of kill using Calton Hit function. Anti-air threat envelops are presented when the target velocity, position and the arrangement of four AAA are varying. Then we have compared the analyzed result using developed model with AEM model of MSA program.

A Case Study on The Drone Battle between Azerbaijan and Armenia

  • Sang-Hyuk Park;Seung-Pil Namgung;Sung-Kwon Kim
    • International Journal of Advanced Culture Technology
    • /
    • v.11 no.3
    • /
    • pp.94-98
    • /
    • 2023
  • This study analyzes the combat case involving military drones during the Azerbaijan-Armenian War, which erupted on September 27, 2020. The background of the war revealed that Azerbaijan extensively and aggressively employed offensive drones, which played a decisive role in reshaping the dynamics of the battlefield. Despite Azerbaijan's GDP of $4.639, which corresponds to the level of a developing country, and its 64th rank in global military strength, the country boldly allocated a significant portion of its budget to develop its drone capabilities in preparation for the war. As a result, Azerbaijan effectively utilized offensive drones acquired from Turkey and Israel to neutralize hundreds of tanks, armored vehicles, artillery units, and air defense systems. The purpose of this study is to examine this context and explore how our Korean military organization can enhance its combat capabilities by developing a drone combat system, thereby enabling an effective response posture against multifaceted threats.

A Study on the Trade-off Analysis of Combat Weight for Conceptual design of a Landing Craft Air Cushion (공기부양상륙정의 개념설계를 위한 전투중량 대안분석 연구)

  • 이제동;신용석
    • Journal of the Korea Institute of Military Science and Technology
    • /
    • v.3 no.1
    • /
    • pp.66-75
    • /
    • 2000
  • The purpose of this study is to develop and illustrate methods of applying trade-off techniques to landing craft air cushion design evaluation. The problem areas of concern are the application of quantitative analytical methods to conceptual design. The interrelationships between composite system measures and selected performance requirements(speed, cruising range, cargo etc.) are analyzed and the expressions for gross weight are developed as functions of performance parameters. Trade-offs of performance parameters in terms of weight are then calculated. The application of these results to evaluation of Require Operational Capabilities are illustrated.

  • PDF