发明名称 METHOD AND DEVICE FOR AUTOMATICALLY ESTIMATING PARAMETERS RELATING TO A FLIGHT OF AN AIRCRAFT
摘要 The estimation device comprises an estimation assembly for determining a corrected estimated incidence, with the aid of an estimated incidence which is computed on the basis of aerodynamic parameters and of inertial parameters related to the aircraft and of a measured incidence which is determined on the basis of measurements carried out on the aircraft by at least one incidence probe. This estimation device thus makes it possible to obtain estimations of the speed of the aircraft, of its incidence and of the total temperature, on the basis of aerodynamic and inertial parameters.
申请公布号 US2016178364(A1) 申请公布日期 2016.06.23
申请号 US201514658594 申请日期 2015.03.16
申请人 Airbus Operations S.A.S. 发明人 WALTER Stéphane
分类号 G01B21/22;B64D43/00 主分类号 G01B21/22
代理机构 代理人
主权项 1. A method for automatically estimating at least one parameter related to a flight of an aircraft, including at least one incidence of the aircraft, the method comprising at least one first series of successive steps for automatically determining a corrected estimated incidence, the first series of successive steps comprising, in an automatic and iterative manner: a) computing an estimated incidence on the basis of aerodynamic parameters and of inertial parameters related to the aircraft; b) measuring an incidence of the aircraft;c) verifying whether the measured incidence is considered to be consistent or inconsistent;d) as a function of the verification carried out in step c): as long as the measured incidence is considered to be consistent, in determining a correction value and in adding this correction value to said estimated incidence to obtain the corrected estimated incidence; andas soon as the measured incidence is considered to be inconsistent, and as long as this remains the case, in adding a fixed corrective value to said estimated incidence to obtain the corrected estimated incidence.
地址 Toulouse FR