摘要
导引律的设计在导弹制导与控制中具有重要作用,为了解决增广比例导引中导弹-目标视线角速度和视线角加速度不易获得的问题,设计了一种基于高阶滑模微分器的增广比例导引律。首先,根据高阶滑模微分器的数学模型建立视线角速度和视线角加速度的估计模型;其次,根据视线角速度和视线角加速度的估计值,利用一种光滑无抖阵滑模微分器构造增广比例导引律。最后,通过仿真验证表明,具有滑模微分器结构的增广比例导引律导引性能良好。
The design of guidance law plays an important role important role in the missile guidance and control,a new approach of constructing augmented proportion navigation(APN),based on high order sliding differentiator(HOSD),is designed to solve the problem that it is difficult to obtain the light of sight angle velocity and acceleration.First,estimation model of Light of sight angle velocity and acceleration are established in terms of mathematical model of high order sliding differentiator.Second,augmented proportion navigation(APN)using a terse fast HOSD without chattering is constructed according to the estimation value.Finally,simulation results show that APN with HOSD has good guidance performance.
作者
杨丹丹
方洋旺
彭维仕
杨鹏飞
YANG Dan-dan;FANG Yang-wang;PENG Wei-shi;YANG Peng-fei(School of Aeronautics and Astronautics Engineering,Air Force Engineering University,Xi’an 710038,China;School of Equipment Engineering,Armed Police Force Engineering University,Xi’an 710086,China)
出处
《火力与指挥控制》
CSCD
北大核心
2017年第4期58-62,共5页
Fire Control & Command Control
基金
国家安全重大基础研究基金资助项目(613271030202
15613271030202)
关键词
增广比例导引
高阶滑模微分器
视线角速度
视线角加速度
augmented proportion navigation
high order sliding differentiator
light of sight angle velocity
light of sight angle acceleration