摘要
本文提出了1种旋转导弹纵、侧向运动交连的解耦方法。借助于3自由度陀螺,设置1个“陀螺补偿角”,使导弹在飞行弹道上实现平均解耦。并用'Powell'法进行参数优选。
A method for decoupling the longitudinal and lateral motions of rolling missiles is presented in this paper, in order to realize an average decoupling of the guided missile motions along the whole trajectory,a compensation angle can be set using a three-degree-of-freedom gyro. In addition, design parameters are optimized by Powell's method.
出处
《北京理工大学学报》
EI
CAS
CSCD
1989年第2期41-50,共10页
Transactions of Beijing Institute of Technology
关键词
飞行力学
导弹
弹道
解耦
旋转导弹
flight mechanics, guidance, guided missile trajectories, cross coupling/rolling missile, decoupling.
