A Fast-Solving Method of Allowable Attack Area of Air-to-Surface Guided Bombs

doi:10.3969/j.issn.1000-1093.2012.04.002

Abstract

Abstract: A new solving method called local accurate search was proposed for the calculation of allowable attack area of air-to-surface missiles. Compared with traditional method, the local accurate search can search the area online and reduce the time of search with the required precision. The new method employs the local search to find an accurate result by combining the traditional flight range table with the model calculation method, which meets the requirements for attacking of moving target and fast calculation.

Key words: control and navigation technology of aerocraft, allowable attack area, fast calculation, online search

CLC Number:

TJ765.3

LI Qiang, XIA Qun-li, CUI Ying-ying, WEN Qiu-qiu. A Fast-Solving Method of Allowable Attack Area of Air-to-Surface Guided Bombs[J]. Acta Armamentarii, 2012, 33(4): 390-394.

References

［1］刘代军,高晓光,李言俊, 等. 中远程空空导弹允许攻击区的快速模拟算法[J]. 西北工业大学学报, 1999, 17(4)：530-533.
LIU Dai-jun, GAO Xiao-guang, LI Yan-jun, et al. A fast simulation algorithm for calculating the allowable attack area for air to air missiles[J]. Journal of Northwestern Polytechnical University, 1999, 17(4): 530-533. (in Chinese)
［2］杜昌平, 周德云, 江爱伟. 一种空空导弹可攻击区快速算法[J]. 西北工业大学学报, 2006, 24(6)：682-685.
DU Chang-ping, ZHOU De-yun, JIANG Ai-wei. A better method for computing air-to-air missile trajectory[J]. Journal of Northwestern Polytechnical University, 2006, 24(6): 682-685. (in Chinese)
［3］张有济. 战术导弹飞行力学设计[M]. 北京：宇航出版社，1998:58-72.
ZHANG You-ji. Tactical missile flight dynamics design[M]. Beijing: Astronautic Press, 1998:58-72. (in Chinese)
［4］钱杏芳, 林瑞雄, 赵亚男. 导弹飞行力学[M]. 北京: 北京理工大学出版社, 2003: 86-111.
QIAN Xing-fang, LIN Rui-xiong, ZHAO Ya-nan. Missile flight dynamics[M]. Beijing: Beijing Institute of Technology Press, 2003: 86-111. (in Chinese)
［5］约瑟 J. 哲尔格尔. 系统工程初步研究[M]. 史超礼, 译. 北京: 国防工业出版社, 1965:157-165.
Joseph J. Siegel Gyor. System preliminary design[M]. SHI Chao-li, translated. Beijing: National Defense Industry Press, 1965: 157-165. (in Chinese)
［6］ Garnell P. Guided weapon control systems[M]. London: Royal Military College of Science Press, 2004:161-172.
［7］解可新, 韩立兴. 最优化方法[M]. 天津：天津大学出版社，2002:60-65.
XIE Ke-xin, HAN Li-xing. Optimization methods [M]. Tianjin: Tianjin University Press，2002:60-65. (in Chinese)
［8］张平, 方洋旺, 金冲，等. 空空导弹攻击区实时解算的新方法[J]. 弹道学报, 2010, 22(4)：11-14.
ZHANG Ping, FANG Wang-yang, JIN Chong, et al. A new method of real-time calculation for attack area of air-to-air missile[J]. Journal of Ballistics, 2010, 22(4):11-14. (in Chinese)

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