发明名称 LOW VISIBILITY LANDING SYSTEM
摘要 Examples of the present invention may include a low visibility landing system for guiding aircraft on landing approaches. The low visibility landing system may aid a pilot during landing in low visibility conditions such that an aircraft may descend to lower altitudes without visual contact with the runway than is possible with other landing systems. The system may use various navigational systems to produce a hybrid signal that may be more stable than individual signals of those navigational systems. The hybrid signal is compared to a predetermined landing approach plan to determine the deviation of the aircraft from the landing approach plan and to provide guidance to the pilot to get the aircraft back onto the landing approach plan. The system may also use multiple navigational systems to perform checks on an operation of a primary navigational system to ensure that the primary navigational system is operating accurately.
申请公布号 US2011106345(A1) 申请公布日期 2011.05.05
申请号 US20090611645 申请日期 2009.11.03
申请人 TAKACS ROBERT S;FREEMAN GARY M 发明人 TAKACS ROBERT S.;FREEMAN GARY M.
分类号 G05D1/00;G05D1/10;G06F19/00 主分类号 G05D1/00
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