SYSTEMS AND METHODS FOR PRODUCING TWO INDEPENDENT DISSIMILAR ATTITUDE SOLUTIONS, TWO INDEPENDENT DISSIMILAR INERTIAL SOLUTIONS OR BOTH FROM ONE IMPROVED NAVIGATION DEVICE

Systems and methods for producing two independent dissimilar attitude solutions, two independent dissimilar inertial solutions or both from one improved navigation device are disclosed. In one embodiment, an avionics system comprises: an inertial navigation device configured to produce a first set o...

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Bibliographische Detailangaben
Hauptverfasser: MILLER MICHAEL G, HORNER ADAM ROSS
Format: Patent
Sprache:chi ; eng
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