发明名称 Navigation aid method for determining the path of an aircraft
摘要 Navigation aid method for determining, by an instruction giver, the path of an aircraft initially following a predetermined path in an approach phase and upon which are defined a safety altitude and an alarm limit, said aircraft including a navigation system of the INS/GNSS type including a satellite information receiver and at least one inertial unit producing position information, said method including determining a future path; estimating predicted protection radii on the future path are estimated, starting at the calculation time in the case of a critical situation, in terms of position information, which starts at the calculation time; calculating a limit time after which the predicted protection radius is greater than or equal to the alarm limit; and calculating a limit time after which the predicted protection radius is greater than or equal to the alarm limit.
申请公布号 US9046894(B2) 申请公布日期 2015.06.02
申请号 US201013266649 申请日期 2010.04.27
申请人 Thales 发明人 Bouniol Pierre;Polaert Olivier;Clemenceau Pierre-Jérôme
分类号 G05D1/10;G05D1/06;G08G5/02;G01C21/12;G05D1/00 主分类号 G05D1/10
代理机构 Baker & Hostetler LLP 代理人 Baker & Hostetler LLP
主权项 1. A navigation aid method for determining, by an instruction giver, the path of an aircraft initially following a predetermined path in an approach phase and upon which are defined a safety altitude and an alarm limit, said aircraft comprising a navigation system of an Inertial Navigation System/Global Navigation Satellite System (INS/GNSS) type comprising a satellite navigation receiver and at least one inertial unit, said method comprising: determining a current position of the aircraft; determining a future path of the aircraft from the current position; estimating a predicted protection radii on the future path, starting at a calculation time in a case of a critical situation, in terms of a loss of GNSS position information, which starts at the calculation time; calculating a limit time after which the predicted protection radius is greater than or equal to the alarm limit; calculating a limit extraction time that corresponds to a maximum time after which the aircraft must leave the predetermined path in order to be able to reach the safety altitude by the time limit; and transmitting the value of the limit extraction time to the instruction giver.
地址 Courbevoie FR