MANAGEMENT OF ALTERNATIVE ROUTES FOR AN AIRCRAFT
First Claim
1. A method for managing a route of an aircraft, implemented in a system comprising an avionic system and a non-avionic system, comprising the steps:
- determining an alternative route to the current route in the non-avionic system;
receiving an authorization to insert said route into the avionic flight management system; and
inserting said route into the avionic flight management system.
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Accused Products
Abstract
Various methods for regulating and/or for integrating avionic systems with non-avionic systems are described. An avionic system is generally associated with a physical fault rate that is lower and a logic verification that is higher than those of a non-avionic system. Developments describe notably the use: of remote computing resources; of comparison, test, verification and authorization steps before injection of data of non-avionic origin into the avionics; of human-machine interaction methods; of various parameters (weather, air traffic, etc.) for the purpose of combinatorial optimization; and of electronic flight bags EFB and of flight management systems FMS.
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Citations
15 Claims
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1. A method for managing a route of an aircraft, implemented in a system comprising an avionic system and a non-avionic system, comprising the steps:
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determining an alternative route to the current route in the non-avionic system; receiving an authorization to insert said route into the avionic flight management system; and inserting said route into the avionic flight management system. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13)
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14. A system for managing a route of an aircraft, comprising
a non-avionic system configured to determine one or more alternative routes to the current route of the aircraft; -
a gateway system configured to receive an authorization to insert an alternative route into an avionic system; said avionic system comprising a flight management system configured to insert said route into the avionic flight management system; the avionic system being associated with a physical fault rate that is lower and a logic verification that is higher than those of a non-avionic system. - View Dependent Claims (15)
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Specification