首页>
外国专利>
FLIGHT CONTROL SYSTEM AND METHOD FOR A CONVERTIBLE FIXED-WING DRONE PROVIDING A STABILIZED CONTINUOUS TRANSITION BETWEEN A VERTICAL STATIONARY FLIGHT AND A HORIZONTAL CRUISE FLIGHT
FLIGHT CONTROL SYSTEM AND METHOD FOR A CONVERTIBLE FIXED-WING DRONE PROVIDING A STABILIZED CONTINUOUS TRANSITION BETWEEN A VERTICAL STATIONARY FLIGHT AND A HORIZONTAL CRUISE FLIGHT
展开▼
机译:在垂直静止飞行和水平巡航飞行之间提供稳定的连续过渡的可旋转固定翼无人机的飞行控制系统和方法
展开▼
页面导航
摘要
著录项
相似文献
摘要
A flight control system is configured to control the flight of a convertible fixed-wing drone (12), having two left and right wings, each supporting a propeller in front and a deflection flap at the rear edge. The control system includes an attitude regulator (154) of the drone (12) to respectively control the roll angles ϕm, pitch θ m and yaw Ψm, measured by one or more sensors on setpoint angles ϕd, pitch θ d and lace Ψd. The first attitude regulator (154) comprises a first MFC SISO device (162) for modelless control at one input-one output for regulating and controlling the pitch angle θ m measured on the pitch set angle θ d by determining a first command δn for symmetrical deflection of the left and right flaps, applied with the same sign to said left and right flaps.
展开▼