曲射攻顶自寻的反坦克导弹制导控制规律研究
Study of Curved Trajectories and Top-attacking Homing Anti-tank Missile's Guidance Law
Received date: 2018-05-10
Online published: 2025-05-20
王磊 . 曲射攻顶自寻的反坦克导弹制导控制规律研究[J]. 弹箭与制导学报, 2019 , 39(2) : 44 -47 . DOI: 10.15892/j.cnki.djzdxb.2019.02.011
Without use of the special distance measurment device, the projectile distance estimation algorithm using the measurement information of imaging seeker and the attitude gyroscope is proposed. And the influence of different interference conditions on the accuracy of the algorithm is analyzed. The guidance control law which is suitable to trajectory control is established, and realiezed the autonomous control of the turning point in the vertical plane of the missile. Through simulation calculation, it is verified that the projectile distance estimation algorithm and control law can meet the requirements of the curved trajectory design.
Key words： homing; anti-tank missile; guidance law; missile and target distance
| [1] | 赵军民, 常冠男, 郭晓辉. 基于战场数字地图信息的反坦克导弹飞行弹道规划方法[J]. 弹箭与制导学报, 2017. 37 (5): 52- 55. |
| [2] | 王爽英, 蒲小平, 魏建峰,等; 在反坦克导弹武器操控系统设计中广泛应用人因工程学理论[J].弹箭与制导学报,2016,36(5):14-16. |
| [3] | 王宝和, 赵志敏. 飞行器三自由度制导控制仿真及应用[J]. 兵器装备工程学报, 2018, 39(10): 44-48. |
| [4] | 吕鸿鹏, 骆强, 孙卫平,等. 基于引战配合的弹目交会毁伤概率仿真研究[J]. 兵器装备工程学报, 2017, 38(6): 33-36. |
| [5] | 李宏宇, 王旭刚. 导引头动力学滞后下带落角约束的最优制导律. 兵器装备工程学报, 2018, 39(7): 40-44. |
| [6] | GARNELL P. Guided Weapon Control Systems [M]. Beijing: Beijing Institule of Technology, 2004: 302 - 306. |
| [7] | 赵勋杰, 高稚允. 光电被动测距技术[J]. 光学技术, 2003,29(6):652-656. |
| [8] | 祁载康, 曹翟, 张天桥,等. 制导弹药技术[M]. 北京: 北京理工大学出版社, 2002: 40-52. |
| [9] | 钱杏芳, 林瑞雄, 赵亚男. 导弹飞行力学[M].北京: 北京理工大学出版社, 2000: 28-48. |
| [10] | 万春熙. 反坦克导弹设计原理[M]. 北京: 国防工业出版社, 1981: 140 – 193. |
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