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    METHOD AND SYSTEM FOR INTEGRATING ENGINE CONTROL AND FLIGHT CONTROL SYSTEM
    8.
    发明申请
    METHOD AND SYSTEM FOR INTEGRATING ENGINE CONTROL AND FLIGHT CONTROL SYSTEM 有权
    集成发动机控制和飞行控制系统的方法和系统

    公开(公告)号：US20130054055A1

    公开(公告)日：2013-02-28

    申请号：US13221102

    申请日：2011-08-30

    申请人： Harry Kirk Mathews, JR. ,  Sridhar Adibhatla ,  Jeffrey Russell Bult

    发明人： Harry Kirk Mathews, JR. ,  Sridhar Adibhatla ,  Jeffrey Russell Bult

    IPC分类号： G05D1/00 ,  G06F19/00

    CPC分类号： B64C19/00 ,  B64D31/06 ,  F05D2260/80 ,  H04B7/18506

    摘要： A method and system of operating an aircraft system are provided. The aircraft system includes an integrated aircraft flight control system that includes an engine control system configured to generate engine performance and health information. The integrated aircraft flight control system also includes a flight control system configured to generate flight information and trajectory intent information. The integrated aircraft flight control system further includes a communications channel communicatively coupled between the engine control system and the flight control system, where the engine control system is configured to transmit the generated engine performance and health information to the flight control system using the communications channel and the flight control system is configured to transmit the generated flight information and trajectory intent information to the engine control system using the communications channel.

    摘要翻译： 提供了一种操作飞行器系统的方法和系统。 该飞行器系统包括集成的飞行器飞行控制系统，其包括被配置为产生发动机性能和健康信息的发动机控制系统。 综合飞行器飞行控制系统还包括配置成产生飞行信息和轨迹意图信息的飞行控制系统。 集成飞行器飞行控制系统还包括通信地耦合在发动机控制系统和飞行控制系统之间的通信通道，其中发动机控制系统被配置为使用通信通道向飞行控制系统发送生成的发动机性能和健康信息，以及 飞行控制系统被配置为使用通信信道将所生成的飞行信息和轨迹意图信息发送到引擎控制系统。