This demonstration models a flight control for the longitudinal motion of a Grumman Aerospace F-14 Tomcat. First order linear approximations of the aircraft and actuator behavior are connected to an analog flight control design that uses the pilot

The performance coefficient depends on both the pitch angle (β) and the tip speed ratio (λ). The tip speed ratio is calculated by using blade tip speed and wind speed upstream of the rotor. The relationship between performance coeffi cient (c_

永磁直驱风力发电系统，含最大风力追踪，桨距角控制。简单模型-Permanent magnet direct drive wind power generation system, including maximum wind track, the pitch angle control. Simple Model

DFIG wind system with pitch angle controland reactive power control