摘要
针对防空反导用中口径舰炮制导炮弹动力学建模和动态特性,借鉴旋转导弹单通道控制的研究方法,在常规火箭弹外弹道模型的基础上建立有控弹道模型,对有控弹道模型进行线性化,并推导出短周期扰动运动弹体传递函数。仿真结果表明,在输入控制力的作用下,传递函数可应用于分析中口径舰炮制导炮弹在有控作用下的飞行稳定性与操纵性。
Aiming at the dynamic - modeling and dynamic characteristics of medium caliber naval gun guided projectile for air defense and anti - missile and drawing on the research method of a rotary rocket＇ s single channel control, the paper builds a controlled ballistic missile model. The simulation re- sult shows, under the input controlling force, transfer function can be used to analyze flight stability and maneuverability of the medium caliber naval gun guided projectile under control.
出处
《长沙航空职业技术学院学报》
2012年第4期41-45,共5页
Journal of Changsha Aeronautical Vocational and Technical College
关键词
反导
中口径舰炮
制导炮弹
弹道模型
动态特性
anti -missile
medium caliber naval gun
guided projectile
ballistic missile model
dynamic characteristics
