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 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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