发明名称 ROTOR MOMENT FEEDBACK FOR STABILITY AUGMENTATION
摘要 Embodiments are directed to obtaining at least one measurement of blade bending associated with at least one blade of at least one rotor of an aircraft, processing, by a device comprising a processor, the at least one measurement to obtain moment data, obtaining data from an inertial measurement unit (IMU), and processing, by the device, the moment data and the data from the IMU to generate a command configured to stabilize the aircraft.
申请公布号 WO2015156879(A3) 申请公布日期 2016.04.07
申请号 WO2015US11906 申请日期 2015.01.19
申请人 SIKORSKY AIRCRAFT CORPORATION 发明人 ELLER, EREZ;WULFF, OLE
分类号 B64C27/57;B64C27/78;B64C27/80;G01L5/00 主分类号 B64C27/57
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