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飞翼布局飞机由于采用了翼身融合技术和无尾布局,具有隐形特性,军事和民用的应用潜力十分巨大。由于飞翼布局飞机本体静稳定性差,航向又不稳定,不易操纵,因此需要解决控制律和多操纵面的协调控制技术。以一种大展弦比飞翼布局模型验证机为研究对象,开展了大展弦比飞翼布局无人机的飞行控制技术研究。通过仿真手段,验证了所提出的飞翼布局无人机的飞行控制及多操纵面协调控制技术的合理性。
Flying wing layout Aircraft due to the use of wing fusion technology and tail layout, with stealth features, military and civilian applications have great potential. Because of the poor static stability of the flying wing layout aircraft body, the course is not stable, not easy to manipulate, so need to solve the control law and multi-control surface coordination control technology. With a large aspect ratio flying wing layout model verification machine as the research object, a large aspect ratio flying wing layout UAV flight control technology research. Through the simulation, the rationality of the proposed flight control and multi-control surface coordinated control technology of the flying wing layout UAV is verified.