发明名称 Procedimiento y sistema de guiado de aviones
摘要 The present invention relates to a system and method for steering aircraft along a predetermined track. Particularly, but not exclusively, the invention relates to steering an aircraft along a lateral path (e.g. a track described by reference to latitude and longitude) by a method comprising: calculating a nominal track correction; providing an upper limit and a lower limit for the nominal track correction; setting a desired track correction as: (i) the nominal track correction if the nominal track is between the upper limit and the lower limit; (ii) the upper limit if the nominal track correction is greater than or equal to the upper limit; or (iii) the lower limit if the nominal track correction is less than or equal to the lower limit; and steering the aircraft using the desired track correction.
申请公布号 ES2458294(T3) 申请公布日期 2014.04.30
申请号 ES20110382311T 申请日期 2011.10.04
申请人 THE BOEING COMPANY;THE BOEING COMPANY 发明人 D'ALTO, LUIS P.;GRABOW, CHRISTIAN
分类号 G05D1/04;G05D1/06 主分类号 G05D1/04
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