Hybrid synthetic aircraft landing system

Details Hybrid synthetic aircraft landing system Hybrid synthetic aircraft landing system

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01

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G01S 1/06 (2006.01) G01C 23/00 (2006.01) G01S 1/08 (2006.01) G01S 1/14 (2006.01) G05D 1/06 (2006.01) G08G 5/02 (2006.01)

Patent

CA 2136570

An avionics device, associated with an aircraft landing system, capable of being operated in conjunction with externally transmitted signals including a portion for receiving the externally transmitted signals. There is an additional portion which determines state vector information based solely upon the externally transmitted signals.

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