Journal of Projectiles, Rockets, Missiles and Guidance >
Fading Memory Filter-based Impact Point Prediction of Trajectory Correction Projectile
Received date: 2014-03-19
Online published: 2025-05-26
Trajectory correction projectiles (TCP) require to predict impact point rapidly for control system design, the truth is that it's impossible to depict real motion of projectile with motion equation. The application of fading memory filter was proposed for impact point prediction. Based on trajectory model and impact point prediction equation, the fading memory filter-based impact point prediction equation was presented. Semi-physical simulation and flight test were carried out based on the method, the results show that the method can filter the date real-time, when the projectile trajectory is corrected, the filtered impact point prediction value will change from one state to another smoothly, it's proved that this method can be used in impact point prediction of TCP.
LI Chaowang , GAO Min , FANG Dan , LU Zhicai . Fading Memory Filter-based Impact Point Prediction of Trajectory Correction Projectile[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2015 , 35(3) : 134 -137,142 . DOI: 10.15892/j.cnki.djzdxb.2015.03.034
| [1] | 申强, 葛腼, 张冀兴, 等. 一种 GPS 弹道辨识方法的精度仿真分析[J]. 北京理工大学学报, 2009, 29(2):100-102. |
| [2] | Thomas Recchia. Projectile velocity estimation using aero-dynamics and accelerometer measurements: A kalman filter approach[R]. U. S. Army ARDEC, METC, 2010. |
| [3] | 李岩, 任睿, 王旭刚, 等. 两种卡尔曼滤波模型在修正弹弹道数据处理中的应用比较[J]. 弹道学报, 2011, 23(1):27-30. |
| [4] | 丁传炳, 王良明, 常思江, 等. 卡尔曼滤波在GPS制导火箭弹中的应用[J]. 南京理工大学学报, 2010, 34(2):157-160. |
| [5] | Yoshio Kosuge. Non-process-noise tracking filter using a constant velocity model[C] // SICE Annual Conference, 2008. |
| [6] | 杨绍卿. 火箭外弹道偏差与修正理论[M]. 北京:国防工业出版社, 2011. |
| [7] | 陈世年. 固体弹道导弹系列控制系统设计[M]. 北京:宇航出版社出版, 1996. |
| [8] | Paul Zarchan. Tactical and strategic missile guidance[M]. American Institute of Aeronautics, Inc. 1997. |
/
| 〈 |
|
〉 |