Velocity Magnitude Control of Maneuverable Reentry Warhead
In this paper, the kinematic model of reentry warhead was built to verify the effect of control law. Then, an idea velocity curve was designed to support a standard of velocity control and the calculation of attack angle and sideslip angle was discussed. Finally, the efficiency of control law was verified through simulation. The simulation result shows that the control law proposed in this paper can limit the velocity magnitude error within 10m without losing accuracy of control of fall point and velocity direction.
reentry maneuver/Me warhead ideal velocity carve velocity magnitude control supplementary attack angle
Kaifeng Liu Xinxue Liu Fang Wang Jian Wu
Xian Research Institute of High-tech Xian,China
国际会议
The 6th International Forum on Strategic Technology(IFOST 2011)(第六届国际战略技术论坛)
哈尔滨
英文
374-377
2011-08-22（万方平台首次上网日期，不代表论文的发表时间）