收稿日期: 2015-06-06
网络出版日期: 2025-05-23
基金资助
中国博士后科学基金(2013M541676); 江苏省高等职业院校高级访问工程师计划资助项目(2014FG102); 江苏省高校“青蓝工程”基金资助
Research on Control Method for Terminal Correction Mortar Projectiles Subjected to Lateral Impulses Based on Miss Distance Prediction
Received date: 2015-06-06
Online published: 2025-05-23
曹小兵 , 徐伊岑 , 常思江 , 齐斌 . 基于脱靶量预测的脉冲末修迫弹控制方法研究[J]. 弹箭与制导学报, 2017 , 37(2) : 23 -26,31 . DOI: 10.15892/j.cnki.djzdxb.2017.02.006
In view of the control problem of terminal correction mortar projectiles subjected to lateral impulses, a control method based on miss distance prediction was proposed. The impulse control force and control torque were analyzed, and the controlled 6-degree-of-freedom motion equations were deduced. By using the deviation angle and its azimuth information between projectile and target measured by strapdown laser seeker, a miss distance prediction model was established. On this basis, the thruster working mode was designed, also, the methods of determining the number of thrusters needed and the direction of starting control were given. Simulation results indicated that the circular error probable (CEP) was reduced by 80%, and the mean miss distance of the controlled impact points was 7.85 m. It proved that the proposed control method could correct the trajectory deflections effectively and thus improve the hit precision.
| [1] | 中国科学技术协会. 兵器科学技术学科发展报告(2010—2011)[M]. 北京: 中国科学技术出版社, 2011: 93- 99. |
| [2] | JITPRAPHAI T, COSTELLO M. Dispersion reduction of adirect fire rocket using lateral pulse jets[J]. Journal ofSpacecraft and Rockets, 2001, 38 (6): 929- 936. |
| [3] | JITPRAPHAI T, BURCHETT B, COSTELLO M. A com-parison of different guidance schemes for a direct fire rocketwith a pulse jet control mechanism: ADA 401 519[R]. 2002. |
| [4] | 张成. 脉冲修正弹药射程预测控制方法[J]. 弹道学报, 2010, 22 (1): 20- 23. |
| [5] | 曹营军, 高敏. 末修迫弹修正效果影响因素分析[J]. 军械工程学院学报, 2009, 21 (1): 24- 27. |
| [6] | GUPTA SK, SAXENA S, SINGHAL A, et al. Trajectorycorrection flight control system using pulsejet on an artilleryrocket[J]. Defence Science Journal, 2008, 58 (1): 15- 33. |
| [7] | GLEBOCKI R, VOGT R. Guidance system of smart mortarmissile[J]. The Archive of Mechanical Engineering, 2007, 54 (1): 47- 63. |
| [8] | 葛健全, 张晓今, 杨涛, 等. 利用捷联导引头信息实现脉冲比例导引. 弹道学报, 2008, 20 (1): 98- 101. |
| [9] | XU Jinxiang. Study on overall concept planning of terminalcorrection mortar projectiles[J]. Journal of Beijing Institu-te of Technology, 2008, 17 (2): 127- 132. |
| [10] | MALEJKO G, BURKE PJ, DOHRN R, et al. Jet inter-action effect on the precision guided mortar munition(PGMM)[C] // 26th Army Science Conference. Orlan-do, Florida[s.n.], 2008: 1- 6. |
| [11] | 曹小兵. 脉冲末修迫弹弹道特性分析与控制方案设计[D]. 南京: 南京理工大学, 2012. |
| [12] | 韩子鹏. 弹箭外弹道学[M]. 北京: 北京理工大学出版社, 2008: 127- 201. |
/
| 〈 |
|
〉 |