摘要
目的 运用地磁感应传感器对旋转飞行中的多管火箭弹进行控制 .方法 通过分析合理地利用地磁导航系统 ,以实现弹的自动控制程序 .结果 地磁感应传感器与两个线性加速度计的使用将给出足够的信息量以供实现弹的程序控制 .结论 推荐的控制系统性能优于现有的编程控制系统 .
Aim\ To study the control system of the shells, rotating in flight, many pipes jet system with use of the induction sensors of the geoma gnetic filed. Methods\ On the basis of the analysis navigation control system wi th use of the induction sensors for realization program management of the shells . Results\ The geomagnetic induction sensor and two linear acceler ation meters give sufficient volume of the information for realization of the pr ogram way of management. Conclusion\ Offered control system best t han regular control \{system.\}
出处
《测试技术学报》
2001年第3期169-171,共3页
Journal of Test and Measurement Technology
