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[an error occurred while processing this directive]二维弹道修正弹复合制导方法
收稿日期: 2017-09-04
网络出版日期: 2025-05-30
基金资助
国家自然科学基金(11402117);国防“971”计划项目资助
Study on Compound Guidance Method of Two-dimensional Trajectory Correction Projectile
Received date: 2017-09-04
Online published: 2025-05-30
王琦 , 钟扬威 , 王良明 . 二维弹道修正弹复合制导方法[J]. 弹箭与制导学报, 2018 , 38(4) : 20 -22 . DOI: 10.15892/j.cnki.djzdxb.2018.04.005
To solve the trajectory correction problem in two-dimensional trajectory correction projectile deviating from the program trajectory at different angles of incidence, the axis and centroid movement law of two-dimensional trajectory correction projectile under the action of control force are studied. Aiming at the advantages and disadvantages of the guidance method based on velocity direction correction and the guidance method of fall prediction, a two-dimensional correction projectile composite guidance method is proposed. Velocity direction correction guidance method is used at the initial guidance, and fall prediction guidance algorithm is use at the ballistic apex. The simulation results show that the combined guidance method has higher accuracy both at small firing angle and at large firing angle.
| [1] | 韩子鹏. 弹箭外弹道学[M]. 北京: 北京理工大学出版社, 2008: 569-578. |
| [2] | 徐明友. 火箭外弹道学[M]. 哈尔滨: 哈尔滨工业大学出版社, 2004: 299-315. |
| [3] | 常思江, 王中原, 刘铁铮. 鸭式布局双旋弹飞行动力学建模与仿真[J]. 弹道学报, 2014, 26(3): 1-5. |
| [4] | 王中原, 王良明. 修正弹道飞行稳定性分析[J]. 兵工学报, 1998, 19(4): 298-300. |
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