摘要
为了适应未来海战的特点和要求,如何提高反舰导弹的突防能力,已经成为各国研究的一项重点。本文在采用过载控制方案的基础上,采用非线性控制方法,设计了反舰导弹线性自适应变结构复合控制器。在过载稳定回路的基础上,通过对导弹高度和侧向偏移的控制实现了导弹的飞行控制系统设计。通过对导弹的末端机动信号的设计,实现了导弹纵向跃升和航向蛇形两种机动弹道。
Abstract: In order to adapt to characteristic and requirement of the future naval battles, how to improve the penetration capability of anti-ship missile has become an important research of every country. On the basis of overload control, a composite controller of linear/AVSC is designed using the method of nonlinear control in this paper. Its flight control system is designed through the control of height and later- al displacement based on overload stable loop. By designing the maneuverable signal at terminal trajectory of anti-ship missiles, the missile can realize longitudinal climb and snaky trajectory.
出处
《航空兵器》
2011年第5期23-25,55,共4页
Aero Weaponry
关键词
反舰导弹
末端机动弹道
过载控制
anti-ship missile
terminal maneuvering trajectory
overload control