• Title/Summary/Keyword: 지능형 탄약

Search Result 6, Processing Time 0.021 seconds

Development of Flight Control System for Gliding Guided Artillery Munition - Part I : Operational Concept and Navigation (유도형 활공 탄약 비행제어시스템 개발 Part I : 운용 개념 및 항법)

  • Lim, Seunghan;Pak, Changho;Cho, Changyeon;Bang, Hyochoong
    • Journal of the Korean Society for Aeronautical & Space Sciences
    • /
    • v.42 no.3
    • /
    • pp.221-228
    • /
    • 2014
  • In this paper, the operational concept and the navigation algorithms for the gliding guided artillery munition are studied. The gliding guided artillery munition has wings for gliding; therefore spin of the munition should be eliminated. The previous navigation algorithms assumed a spinning munition with constant angular velocity; hence, they cannot be applied for the gliding munition. Moreover, lateral stability becomes worse due to decrease of angular momentum. Therefore, side force should be controlled to improve the stability, and the munition should maneuver, then the previous navigation algorithms for typical fixed-wing aircraft cannot be applied. In this paper, we apply the previous navigation algorithms for the spinning munition. Spin is eliminated and wings are deployed based on the estimation results, and the advanced navigation algorithm for the non-spinning munition is introduced.

155밀리 항력감소 이중목적 고폭탄 개발 의의 및 성과

  • Jo, Dong-Seong
    • Defense and Technology
    • /
    • no.6 s.268
    • /
    • pp.60-65
    • /
    • 2001
  • 21세기 첨단과학기술의 발전과 불특정 위협 그리고 세계적 무기체계 발전추세를 감안한 화포의 사거리 증가는 한계에 도달하고 화력운용개념 또한 정밀타격을 요구하고 있는 상황하에서, K9 신형 155밀리 자주포를 통하여 종심지역의 적 전차 및 인원표적을 공격하는 능력을 갖추며, 지능형 탄약을 개발할 수 있는 기반을 조성하고, 국내 독자적인 장거리 탄약개발기술을 확보했다는 측면에서 개발의의 및 성과가 매우 크다 하겠다. 따라서 한국의 지정학적인 전략적 요충지로서 항상 주변 강대국 위협에 대비하는 전투력을 구비하도록 방위산업체 주도의 무기개발이 일반화되어야 할 것이다.

  • PDF

Development of Flight Control System for Gliding Guided Artillery Munition - Part II : Guidance and Control (유도형 활공 탄약 비행제어시스템 개발 Part II : 유도 및 제어)

  • Lim, Seunghan;Pak, Changho;Cho, Changyeon;Bang, Hyochoong
    • Journal of the Korean Society for Aeronautical & Space Sciences
    • /
    • v.42 no.3
    • /
    • pp.229-236
    • /
    • 2014
  • In this paper, the guidance laws and controllers for the gliding guided artillery munition is studied. The gliding guided artillery munition has wings for gliding to increase a range; therefore previous guidance laws and controllers for the guided munition could not be applied. Concepts of vector field guidance and proportional navigation guidance are applied for mid-term and terminal guidance, respectively. The gliding guided artillery munition is operated within wide altitude and speed areas; therefore, the controllers are designed for each area, and gain-scheduling and the linear interpolation technique is applied to compute the appropriate gains.

Study of Estimation Model for Wartime Stockpile Requirement of Intelligent Ammunition against Enemy Armored Vehicles (장갑차량 공격용 지능형 포탄의 전시 소요량 산정 모형에 관한 연구)

  • Cho, Hong-Yong;Chung, Byeong-Hee
    • Journal of the military operations research society of Korea
    • /
    • v.34 no.2
    • /
    • pp.143-162
    • /
    • 2008
  • This paper aims to formulate the method of estimating the wartime stockpile requirement of 155mm self-propelled artillery including intelligent ammunition for armored vehicles, currently being developed. The usual method of utilizing war-game simulation results in considerable margins in expected occupancy ratio between ground forces and air forces for each weapon system for armored vehicles. Also, the method tends to produce excessive output greater than the minimal stockpile requirements; therefore, the study aims to overcome limitations like these by the allocation method for each weapon system according to targets. This allocation method is better than war-game simulation method.

A Study on the Design Analysis and Test of a Ballute Type Parachute of the Smart Submunition (지능형 자탄의 벌루트형 낙하산 설계 해석 및 시험에 관한 연구)

  • Lee, Sang-Kil;Lee, Sang-Seung
    • Journal of the Korea Institute of Military Science and Technology
    • /
    • v.11 no.2
    • /
    • pp.23-31
    • /
    • 2008
  • The configuration model of a ballute type RAID(Ram Air Inflated Decelerator) for reducing the high speed and high revolution of smart submuntion is designed and tested. Three dimensional incompressible turbulent flow computational fluid dynamic analysis for the assembly of ballute and submunition is performed and pressure distribution, velocity, and drag around the assembly is calculated. Aerodynamic characteristics of the ballute assembly such as air flow inside and outside of the ballute and pressure distribution is clearly shown and it's drag coefficient is computed. Trajectory analysis of the submunition is performed and is in good agreement with the descending trajectory data of experimental model tested.

A Methodology for Applying A.I. to Fire Command & Control System (사격지휘체계의 인공지능 적용 방안)

  • Han, Changhee;Lee, Jong-kwan;Shin, Kyuyong;Choi, Sunghun;Moon, Sangwoo
    • Proceedings of the Korean Society of Computer Information Conference
    • /
    • 2019.07a
    • /
    • pp.5-6
    • /
    • 2019
  • 본 논문에서는 데이터 기반 정보 고도화를 통해, 사격전술지휘 의사결정체계의 Assisted Decision-Maker인 AI 부전포대장을 구현하는 방법론을 제시한다. 전포대장은 지휘결심의 말단에 있는 지휘관으로서, 최종적인 의사결정자이다. 이들의 지휘결심이 보다 견고하고 신속하게 이루어지도록 하는 것이 전쟁 승패에 매우 중요한 요소이다. 화력체계를 언급하는 경우 JMEM 탄약효과가 자주 언급되고 한국형 구축 사업이 아직 진행 중이기도 하지만, 완료되더라도 임의의 지형과 전술상황 각각에 대한 유용성까지를 입증하는 데에는 또 다른 기간과 노력이 요구된다. 본고에서는 AI 플랫폼 구축의 실제 사례가 전무한 상황에서 AI 부전포대장 구축을 위해 필요한 연구의 범위와 그 대상을 살펴보고, 지능형 사격지휘체계의 구축 방안을 제안한다.

  • PDF