针对某升力体高超声速飞行器在超燃冲压发动机工作前后的姿态控制问题，分析了发动机进气道关闭、打开和发动机点火3种状态下的机体气动特性。建立了典型的升力体高超声速飞行器的数学模型。采用分数阶控制器的结构和参数配置方法，设计了飞行器的法向过载控制器。控制器内回路采用极点配置法以改善控制系统的动态特性；外回路采用分数阶控制器来配置控制参数以满足飞行器高精度的姿态控制要求。仿真结果表明3种状态下升力体高超声速飞行器机体姿态均控制在平衡位置的±1°动态范围内。%A method for designing fine attitude controllers is proposed for a certain kind of hypersonic vehicle .The airframe aerodynamics for three conditions were analyzed .The fractional controllers with parameter adjusting con -sidered were put forward.Numerical simulation results and their analysis demonstrated preliminarily that attitude angles were maintained within ±1°,thus proving the effectiveness of the approach proposed .
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