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被动寻的式侵彻炸弹的制导律设计 被引量:1

Design of Guidance Law for Passive Homing Penetrating Bomb
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摘要 针对被动寻的式侵彻炸弹的特点,设计了具有末端落角约束的变结构制导律,并采用将制导指令经过一阶低通滤波器的方法,实现对弹体攻角的估计。将该制导律用于电视制导侵彻炸弹的数学仿真,通过仿真讨论了制导律参数对制导效果的影响。仿真结果表明,该攻角估计方法是可行的,该制导律能够同时满足脱靶量和末端落角的要求,达到侵彻炸弹控制弹着角的目的。 According to the characteristics of passive homing penetrating bomb, the variable-structure guidance law with terminal angular constraint is designed. The bomb's angle-of-attack is estimated by the method that the guidance command passes through a first order filter. The guidance law is used for the simulation of a video-guided penetrating bomb. And through the simulation, the influence of the guidance law parameters on the guidance performance is discussed. The simulation shows that the angle-of attack estimation method is feasible, and that the guidance law can meet the demands for both terminal miss distance and impact angle.
出处 《弹箭与制导学报》 CSCD 北大核心 2006年第2期16-19,共4页 Journal of Projectiles,Rockets,Missiles and Guidance
关键词 被动寻的 侵彻炸弹 制导律 末端落角约束 变结构 攻角估计 passive homing penetrating bomb guidance law terminal angular constraint variable-structure angle-of-attack estimation
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参考文献3

  • 1Kim M and Grider K V.Terminal Guidance for Impact Attitude Angle Constrained Flight Trajectories[J].IEEE Transactions on Aerospace and Electronic Systems,1973,AES-9 (6):852-859.
  • 2Byung S K,Jang G L,Hyung S H,et al.Homing Guidance with Terminal Angular Constraint against Nonmaneuvering and Maneuvering Targets[R].AIAA-97-3474:189-199.
  • 3高为炳.变结构控制的理论及设计方法[M].北京科学出版社,1998..

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