推力矢量飞机试飞技术模拟研究  

Simulation Research of Flight Test Techniques for Thrust Vector Aircraft

作　　者：刘选民[1] 田福礼[2] 俞志刚[3] 

机构地区：[1]西北工业大学航空学院,陕西西安710072 [2]中国飞行试验研究院总工办,陕西西安710089 [3]中国飞行试验研究院飞机所,陕西西安710089

出　　处：《飞行力学》2007年第3期1-4,共4页Flight Dynamics

摘　　要：为研究推力矢量飞机的试飞技术,建立了推力矢量飞机的动力学模型,用动态逆方法设计了4种过失速机动控制律,并在地面飞行模拟器上参考标准评估机动动作集(STEMS)进行了飞行模拟试验研究。试验结果表明,使用的4种过失速机动控制模式没有不可接受的操纵响应,飞机采用推力矢量控制后敏捷性明显提高。在模拟导弹攻击目标时,采用过失速机动控制模式具有明显的优势。For researching the flight test techniques of thrust vector controlled aircraft, dynamic models of thrust vector controlled aircraft were established, four post stall maneuver control laws were designed with the dynamic inverse method, tested and investigated according to a standard evaluation maneuver set（STEMS）. The results show that there are no un-receptible responses when the post stall maneuver modes are applied, and agility is raised significantly. When the missile attack process is simulated, the application of post stall maneuvers provides significant advantages.

关 键 词：推力矢量 过失速机动 试飞技术 飞行模拟试验 

分 类 号：V212.1[航空宇航科学与技术—航空宇航推进理论与工程]