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防空导弹灰色预测制导及其仿真 被引量:1

Grey Predicting Guidance and Simulation of Air Defence Missile
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摘要 在高技术防空作战中,减小防空导弹制导误差是提高射击精度的关键。本文提出一种灰色预测控制,减小制导误差的构想,产时制导。 In high-tech air defence fight, dimnishing guided error of air defence missile is the crux to improve shot precision. This paper put forward a conception of dimnishing guided er- ror by way of grey prediction and control, which can realize predicting control and real guid- ance.
机构地区 炮兵指挥学院
出处 《指挥技术学院学报》 1999年第6期84-88,共5页 Journal of Institute of Command and Technology
关键词 防空导弹 制导 仿真 灰色预测控制 air defence missile grey control guidance
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  • 1周少武,章兢,王耀南.具有不确定性和非线性扰动的时滞关联大系统的鲁棒稳定性条件[J].系统工程理论与实践,2004,24(11):82-87. 被引量:3
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  • 6Talole S E,Banavar R N.Proportional navigation through predictive control[J].Journal Guidance and Control Dynamic,1998,21(6):1004-1006.
  • 7Bezik S,Rusnak I,Grey W S.Guidance of a homing missile via nonlinear goemetric control method[J].Journal of Guidance,Control and Dynamic,1995,18(3):441-448.
  • 8Talole S E,Phadke S B,Singh R K.Predictive homing guidance using time delay control[J].Guidance Navigation and Control Conference and Exhibit,California,2005,6159:1-9.
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  • 10Vincent C L.Time-to-go estimate for missile guidance[C]// Guidance,Navigation,and Control Conference and Exhibit,Rhode Island,2005:1-15.

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