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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 s stick pitch command as the set point for the aircraft s pitch attitude and uses aircraft pitch angle and pitch rate to determine commands. A simplified Dryden wind gust model is incorporated to perturb the system.
Update : 2008-10-13 Size : 11.63kb Publisher : wanghuixia

一个F-16仿真程序,可用于一般的飞行器仿真实验.采用了模块化设计.-an F-16 simulation program can be used for general aircraft simulation. Using a modular design.
Update : 2025-02-17 Size : 101kb Publisher : 高旭生

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 s stick pitch command as the set point for the aircraft s pitch attitude and uses aircraft pitch angle and pitch rate to determine commands. A simplified Dryden wind gust model is incorporated to perturb the system.
Update : 2025-02-17 Size : 11kb Publisher : wanghuixia


Update : 2025-02-17 Size : 1.7mb Publisher : 小兔兔牙
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