摘要
针对某远程制导炮弹的弹道特性,讨论分析了该制导炮弹的动态特性及其控制系统设计要求,据此进行了适合于该制导炮弹的自动驾驶仪结构分析和设计,所设计的自动驾驶仪克服了弹体飞行中的低阻尼和动态增益变化大的缺点,能满足该制导炮弹动态性能的要求,仿真结果也说明了这一点。
Aimming at the trajectory characteristics of a guided projectile,it's dynamical response was discussed and design requirments for control system was put forward in the paper. Then reasonalble structure analysis and design for autopilot was given. The autopilot overcomed the faulty of low damping and ingh variation range of dynamical gain of body in flight. The design can meet the requirments of the projectile's dynamical characterises. Such a conclusion was also appoved by simulation result.
出处
《弹箭与制导学报》
CSCD
北大核心
2003年第2期1-4,共4页
Journal of Projectiles,Rockets,Missiles and Guidance
