摘要
讨论了某小型无人机导航系统的设计方案和原理, 阐述了其比例微分式导航控制律设计方法, 分析了其算法的实现。
The scheme and principle of the navigation system of certain mini-UAV is discussed, the design method of the proportion-differential navigation control law is expatiated, and the realizing of the calculating method of the design is analyzed.
出处
《战术导弹技术》
2004年第6期52-54,共3页
Tactical Missile Technology
关键词
控制律
方案
原理
算法
control law
scheme
principle
calculating method
