Journal of Projectiles, Rockets, Missiles and Guidance >
Study of Kinetic Kill Vehicle's Six-degree-of-freedom Simulation Based on the Sliding Mode Guidance Law
Received date: 2013-03-05
Online published: 2025-05-26
To design and research the kinetic kill vehicle's attitude control system, trajectory control system and other system parameters, the six-degree-of-freedom simulation of KKV has been worked out in Matlab's Simulink platform. The ballistic missile also has been intercepted by the sliding mode guidance law. From the results of the simulation, both the attitude control and trajectory control system have been worked out.
GUO Yue , LIU Xinxue , WANG Shunhong . Study of Kinetic Kill Vehicle's Six-degree-of-freedom Simulation Based on the Sliding Mode Guidance Law[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2013 , 33(6) : 38 -41 . DOI: 10.15892/j.cnki.djzdxb.2013.06.023
| [1] | 彭冠一．防空导弹武器制导控制系统设计(上) [M]．北京: 宇航出版社， 1996． |
| [2] | 程国采．战术导弹导引方法[M]．北京: 国防工业出版社， 1996． |
| [3] | 谷良贤，龚春林，郝波．动能拦截器姿控与轨控方案设计及仿真[J]．西北工业大学学报， 2004， 25(3): 402-405． |
| [4] | 王婷，周军． PAC-3 拦截弹建模与仿真研究[J]．系统仿真学报， 2007， 19(20): 4642-4645． |
| [5] | 周荻．寻的导弹新型导引律[M]．北京; 国防工业出版社， 2002． |
| [6] | 闫宝琴，金玉华，李君龙．滑模变结构导引律在动能拦截器上的应用研究[J]．现代防御技术， 2008， 36(1): 59-61． |
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