高超声速飞行器线性变参数一体化式控制律设计

杨庶, 钱云霄, 杨婷

Linear Parameter-Varying Integrated Control Law Design for a Hypersonic Vehicle

YANG Shu, QIAN Yunxiao, YANG Ting

图11 ECEF参考系下高超声速飞行器的姿态四元数响应(水平转弯机动)

Fig.11 Quaternion responses of hypersonic vehicle equations of motion in ECEF reference frame (level turn maneuver)