摘要
建立了质量矩控制导弹的动力学模型,对影响导弹自旋速度变化的主要因素进行了理论和仿真研究,分析了自旋速度变化对控制力矩的影响,并给出了结论。
The dynamics models are presented for mass moment control missile in the paper. Theo-retic analysis, simulation of the main operation ingredients effected roll rate are discussed. On the other hand, theoretic analysis of the changes of the roll rate to the control moment is done. Finally, some conclusions are given.
出处
《航空兵器》
2005年第5期3-6,共4页
Aero Weaponry