sldemo_f14
所属分类:数值算法/人工智能
开发工具:matlab
文件大小:11KB
下载次数:89
上传日期:2008-04-11 15:02:34
上 传 者:
whxrzh
说明: 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.
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sldemo_f14.mdl (60110, 2007-01-21)
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