首页>
外国专利>
METHODS AND SYSTEMS FOR ACTIVE WING AND LIFT SURFACE CONTROL USING INTEGRATED AEROELASTICITY MEASUREMENTS
METHODS AND SYSTEMS FOR ACTIVE WING AND LIFT SURFACE CONTROL USING INTEGRATED AEROELASTICITY MEASUREMENTS
展开▼
机译:集成气动弹性测量方法主动控制机翼和升降机表面的方法和系统
展开▼
页面导航
摘要
著录项
相似文献
摘要
An active wing and lift surface control system for an aircraft is described. The wing and lift surface control system includes an aeroelasticity measurement system configured to provide at least one of real time wing twist measurements and real time measurements of aircraft body bending, at least one actuator mechanically coupled to a control surface of the aircraft, and a control system communicatively coupled to the aeroelasticity measurement system and to the at least one actuator. The control system is operable to receive the measurements from the aeroelasticity measurement system and generate control signals, based on the real time measurements, to operate the at least one actuator to adjust a drag associated with one or more of the wing and the aircraft body.
展开▼