研究了差分gps方法及其在飞机自动着陆控制系统设计中的应用。
It was reported that DGPS (Differential Global Positioning System) method was employed for automatic landing of an aircraft but no technical details are available in the open literature.
使用反馈线性化与改进的模糊控制方法设计飞机纵向自动着陆控制系统。
The control system for longitudinal automatic landing of an aircraft was designed with the methods of feedback linearization and improved fuzzy control.
针对飞翼无人机的特性，利用侧航法和侧滑法设计了侧风着陆控制系统，仿真了系统抗侧风干扰的能力并进行了对比分析。
Based on the characteristics of flying wing UAVs, crosswind landing control systems were designed through the crabbed method and the side-slipping method.
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