Patent ID: 8634972

Claim:
An integrated aircraft flight control system comprising: an engine control system associated with an engine, said engine control system comprising a processor and a memory communicatively coupled to said processor, said engine control system configured to receive engine information from a plurality of sensors associated with the engine and to control a current operation of the engine using the received engine information and to generate engine performance and health information; a flight control system associated with the aircraft, said flight control system comprising a processor and a memory communicatively coupled to said processor, said flight control system configured to receive aircraft information from a plurality of aircraft sensors associated with the aircraft and flight planning information from offboard the aircraft and to generate flight information and trajectory intent information; and a communications channel communicatively coupled directly to said engine control system and said flight control system, wherein said communications channel facilitates transmission of the generated engine performance and health information from said engine control system to said flight control system, wherein said flight control system is configured to modify the operation of the aircraft based on the engine performance and health information generated by the engine control system, wherein said communications channel facilitates transmission of the generated flight information and trajectory intent information from said flight control system to said engine control system, and wherein said engine control system is configured to modify the operation of the engine based on the flight information and the trajectory intent information generated by the flight control system.