HYBRID SYNTHETIC AIRCRAFT LANDING SYSTEM

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 upo...

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Bibliographische Detailangaben
Hauptverfasser:	KLINGENSCHMITT, CARL E, VIVIANI, GARY L
Format:	Patent
Sprache:	eng ; fre
Schlagworte:	AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION CONTROLLING COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS GYROSCOPIC INSTRUMENTS MEASURING MEASURING DISTANCES, LEVELS OR BEARINGS NAVIGATION PARACHUTES PERFORMING OPERATIONS PHOTOGRAMMETRY OR VIDEOGRAMMETRY PHYSICS REGULATING SIGNALLING SURVEYING SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES TESTING TRAFFIC CONTROL SYSTEMS TRANSPORTING
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Beschreibung
Zusammenfassung:	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.