This paper presents a dynamic inversion control method for high Angle - of - attack flight.
提出了一种飞机大仰角飞行的动态逆模糊集成控制方法。
The extended linearization of nonlinear systems is used to design flight control systems at high angle of attack.
利用非线性系统的扩展线性化方法设计具有大迎角的非线性飞行控制系统。
The results of flight test show that JL8 aircraft has very good characteristics of high Angle of attack, low speed and high speed stalls.
试飞结果表明，JL8飞机具有良好的大迎角特性及低速和高速失速特性。
High Angle of attack wind tunnel test techniques is necessary for development of high-maneuverability flight vehicles.
迎角风洞试验技术是先进高机动飞行器研制必需的关键技术。
High Angle of attack wind tunnel test techniques is necessary for development of high-maneuverability flight vehicles.
迎角风洞试验技术是先进高机动飞行器研制必需的关键技术。
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