• Title/Summary/Keyword: Air-to-Surface Guided Bomb

Search Result 2, Processing Time 0.017 seconds

Computation of Launch Acceptability Region of Air-to-Surface Guided Bomb for Moving Target (이동표적에 적용 가능한 공대지 유도폭탄의 투하 가능 영역)

  • Kang, Yejun
    • Journal of the Korean Society for Aeronautical & Space Sciences
    • /
    • v.49 no.7
    • /
    • pp.601-608
    • /
    • 2021
  • Launch Acceptability Region of Air-to-Surface Guided Bomb is defined as the set of release points in order to reach a target successfully. LAR is consisted of fixed target area and moving target area whether the target maneuvers or not. In this paper, the computational algorithm of LAR is studied for fixed and moving target. First, multi-simulations are performed varying platform, target, and atmospheric environment to attain Min/Max DB. Second, the LAR functions are obtained using regression and classification algorithm. For operational suitability, the algorithm for display of LAR is studied to obtain appropriate LAR. In this progress, the results of LAR are suitable to apply air-to-ground guided bomb for moving target.

Computation for Launch Acceptability Region of Air-to-Surface Guided Bomb Using Artificial Neural Network (인공신경망을 이용한 공대지 유도폭탄의 투하가능영역 산출)

  • Kim, Seonggyun;Park, Jeongho;Park, Sanghyuk;Lee, Seoungpil;Kim, Kilhun
    • Journal of the Korean Society for Aeronautical & Space Sciences
    • /
    • v.46 no.4
    • /
    • pp.283-289
    • /
    • 2018
  • Launch Acceptability Region(LAR) means an area for successfully hitting the target. And LAR should be calculated in real time on aircraft so that LAR can be seen by pilot. LAR can be changed by the launch condition of the bomb, the impact condition of the target, and the atmospheric condition at the time of flight of the bomb. In this paper, we propose the calculation method of LAR using Artificial Neural Network(ANN). The learning data was generated by changing each condition from existing LAR model, and LAR model was derived through ANN learning. We confirmed the accuracy of the new LAR model by comparing the difference between the result data of existing LAR model and the new LAR model. And we confirmed the possibility of real time calculation of the LAR model on the aircraft by comparing the calculation time.