Automatic landing system of airplane using adaptive inverse control.
自适应逆控制方法在飞机自动着陆系统中的应用。
This paper presents a novel design procedure for the control of aircraft automatic landing system using nonlinear technique and fuzzy control method.
将非线性控制方法与模糊控制方法相结合对飞机自动着陆系统进行了设计。
The WATCHKEEPER system has been designed for automatic take-off and landing, without the need for pilots during this phase.
“守望者”系统设计了自动起飞和降落，这一过程不再需要飞行员。
The control system for longitudinal automatic landing of an aircraft was designed with the methods of feedback linearization and improved fuzzy control.
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。
DMC-PID bunches control technology in the Angle of attack automatic control system during unpowered flying automatic landing period is introduced.
介绍了将DMC - PID串级控制技术应用到无人机无动力飞行时的自动着陆阶段迎角自动控制系统。
AUTOLAND, Automatic landing using the Digital Flight control System.
自动着陆，使用数字式飞行操作系统来进行自动着陆。
Basic components and operation principals of the automatic carrier landing system are described.
介绍了舰载机自动着舰导引系统的基本组成及工作原理。
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.
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。
Simulation results show that the designed system can satisfy the precision requirement for the longitudinal automatic landing, and has good dynamic and static features.
仿真结果表明，所设计的自动着陆纵向模糊控制系统能满足飞机自动着陆的精度要求，且具有良好的动态、静态特性。
This paper introduced the principle of the automatic carrier landing guidance system and its filtering problem.
介绍了自动着舰导引系统的工作原理及其滤波问题。
Second-order sliding mode controller and automatic carrier landing system is designed. The result of simulation research shows the system has good capability of air attenuation.
仿真对比研究表明二阶滑模控制下的着舰导引系统有较好地抑制气流扰动的能力。
Second-order sliding mode controller and automatic carrier landing system is designed. The result of simulation research shows the system has good capability of air attenuation.
仿真对比研究表明二阶滑模控制下的着舰导引系统有较好地抑制气流扰动的能力。
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