摘要
针对质量矩控制技术的动力学问题,提出了质量矩控制导弹的动力学模型,通过对导弹各参数的理论和数值计算分析,对影响导弹快速响应的主要因素在不同的条件下进行研究,分析了质量矩控制方法迅速改变弹体姿态的能力;在自旋速度满足一定的条件下通过对模型参数的摄动分析,得到质量矩控制导弹的简化动力学模型,仿真分析表明该模型是非线性控制系统分析、设计的基础。
In order to research the dynamic of moving mass actuation missile, the dynamics models are presented for mass moment control missile in the paper. Theoretic analysis, simulation of the main operation ingredients of effecting reaction time is discussed under different condition. Moving mass actuation technique offers significant capability to change missile attitude. Via perturbation method of the modal parameters, the simplified equations are presented on condition that the spin is slow. Simulation results indicate that the models are the basis for the nonlinear control design and analysis.
出处
《系统工程与电子技术》
EI
CSCD
北大核心
2004年第11期1635-1639,共5页
Systems Engineering and Electronics
关键词
质量矩导弹
动力学模型
质量矩控制技术
简化方程
mass moment missile
dynamics models
moving mass actuation technique
simplified equations
