公开(公告)号：US20140371957A1

公开(公告)日：2014-12-18

申请号：US14303430

申请日：2014-06-12

Applicant: THALES

Inventor： Marc RIEDINGER ,  Yannick MERET ,  Julien LOPEZ

IPC: B64F5/00

CPC classification number: B64D45/00 ,  B64D43/00 ,  B64D43/02 ,  G01C23/005 ,  G05D1/0816

Abstract: A method for diagnosis of a loss of control of an aircraft comprises the steps: loading raw data; loading parameters of the aircraft; computing a plurality of reference data comprising a preprocessing comprising for at least one reference datum a sub-step of computing a phase advance term; determining the characteristic thresholds indicative of loss of control; detecting at least one type of loss of control by comparing the reference data with characteristic thresholds; and, when at least one type of loss of control is detected: identifying the type of priority loss of control corresponding to the type of loss of control exhibiting the highest priority level, and communicating the type of priority loss of control to a crew.

Abstract translation: 用于诊断飞机失控的方法包括以下步骤：加载原始数据; 飞机装载参数; 计算包括预处理的多个参考数据，所述预处理包括用于计算相位超前项的子步骤的至少一个参考数据; 确定指示失控的特征阈值; 通过将参考数据与特征阈值进行比较来检测至少一种类型的控制丢失; 并且当检测到至少一种类型的控制失败时：识别与显示最高优先级的控制类型的丢失类型相对应的控制优先级丢失类型，并将控制的优先级丢失类型传达给船员。