Predictive aircraft flight envelope protection system
A protection system, aircraft technology, applied in traffic control systems, control/regulation systems, instruments, etc., to solve problems such as inability to land, aircraft losing flight envelope protection, regardless of gross weight effects or engine failure conditions
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[0030] The following detailed description is merely exemplary in nature and is not intended to limit the invention or the application and uses of the invention. Furthermore, there is no intention to be bound by any theory presented in the preceding background section or the following detailed description.
[0031] introduction
[0032] The disclosed aircraft flight envelope protection system uses flight path prediction techniques to provide a unified full envelope protection that operates over a full range of aircraft flight conditions for a full range of different types of hazards. A flight path prediction is continuously calculated from the current condition of the aircraft using a kinetic energy model. A plurality of predicted trajectories are computed, each representing a different escape route that enables recovery from the hazard when the hazard's threshold or trigger point is reached. The system considers different types of hazards, some involving inherent properties ...
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