A flight control system and method of executing an emergency response for a rotary-wing aircraft includes at least some of a flight control computer in communication with flight control systems and emergency control systems. One or more sensors are used to monitor and detect flight conditions. A method, a computer program product, and a system for detecting a flight emergency and executing solutions for the emergency is described. Embodiments of the present invention describe a method comprising: receiving a sensor alert, executing an alert solution associated with the sensor alert, determining flight condition, determining flight condition is a crash condition, and regulating performance of a main rotor engine and a tail rotor engine.
FLIGHT CONTROL SAFETY SYSTEM
2020-06-18
Patent
Electronic Resource
English
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