期刊文献+

中远程防空导弹的末制导律设计与仿真 被引量:2

Design and Simulation for Terminal Guidanc Law of Long Range Antiaircraft Missile
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摘要 应用线性二次高斯调节器原理,本文提出一种适用于脉冲多卜勒雷达自寻的制导导弹的适应性强,制导精度高,易实现的最优制导规律。为解决工程实现的关键问题,提出了目标机动加速度模型。根据机动目标的统计模型和非线性最优滤波理论推导出一个快速跟踪的自适应滤波算法,并给出了目标机动加速度、导弹与目标相对距离和距离变化率的估计算法。某改进后导弹的仿真结果表明该算法具有很好收敛性和稳定性。 By using the design method of the Linear Quadratic Regulator, for pulse Doppler radar homing missile, a new optimal law, which is of good adaptability, high precision and easy realization for attacking maneuvering target is derived. To resolve the important key in engineering application, an adaptive statistical model of target maneuvering is proposed. Based on the statistical model of target maneuvering and nonlinear Kalman filter, a new adaptive filter algorithm, which can rapidly track and estimate maneuvering acceleration of the target, the velocity and the distance between the missile and the target is proposed. The simulation for a certain improved missile control and guide system shows that the algorithm is stable and has good convergence property.
出处 《系统仿真学报》 EI CAS CSCD 2001年第6期777-780,共4页 Journal of System Simulation
关键词 中远程防空导弹 末制导律 设计 仿真 Homing missile target state estimator maneuvering target guidance law
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参考文献3

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共引文献15

同被引文献18

  • 1徐斌.“爱国者”系列地空导弹[J].地面防空武器,2004(3):19-24. 被引量:9
  • 2葛致磊,周军.远程地空导弹直接力/气动力复合控制技术研究[J].弹箭与制导学报,2005,25(2):42-44. 被引量:8
  • 3邹晖,陈万春,殷兴良.具有侧向推力控制的自旋导弹建模与仿真[J].计算机仿真,2005,22(7):32-35. 被引量:2
  • 4郝丽杰,姚郁,姜宇.质量矩控制导弹的建模与仿真研究[J].系统仿真学报,2005,17(9):2054-2056. 被引量:7
  • 5尚磊云,唐硕,王卫华,杨剑影.空面导弹系统的建模与仿真[J].系统仿真学报,2006,18(3):771-773. 被引量:9
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  • 9Li-Chen Fu, Chi-Wang Tsai, Fu-Kuang Yeh. A Nonlinear Missile Guidance Controller with Pulse Type Input Devices [C]// Proceedings of the American Control Conference (S0743-1619), California, USA: American Automatic Control Council, 1999,3753-3757.
  • 10D Emeliyanov, E Rubinovich, B Miller. Advanced Guidance Law Design Based on the Information-set Concept [C]// Proceedings of the 40th IEEE Conference on Decision and Control (S0-7803-7061-9), Orlando, Florida USA: IEEE, 2001,652-657.

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