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    • 2. 发明申请
    • AIRCRAFT AUTORECOVERY SYSTEMS AND METHODS
    • 飞机自动化系统和方法
    • WO2005083540A1
    • 2005-09-09
    • PCT/US2004/012235
    • 2004-04-21
    • HONEYWELL INTERNATIONAL INC.BATEMAN, Charles, D.JOHNSON Steven, C.GLOVER, John, H.
    • BATEMAN, Charles, D.JOHNSON Steven, C.GLOVER, John, H.
    • G05D1/00
    • G05D1/0061
    • Methods and systems for performing auto-recovery for an aircraft (20). An example system includes position and information systems (26, 30), an automatic flight control system (36), a database (32), and a processor (22). The database includes terrain data, airport data, obstacle data, and protected airspace data. The processor determines if one of a caution alert exists based on data stored in the database and information received from the position and information systems. Auto­recovery instructions are generated and sent to the automatic flight control system if no positive flight control input has been performed at time of expiration of a waiting period. Auto-recovery instructions are generated based on an analysis of two or more auto-recovery routes. The system does not perform auto-recovery if components of the system fail to meet a predefined validity or integrity level.
    • 执行飞机自动恢复的方法和系统(20)。 示例系统包括位置和信息系统(26,30),自动飞行控制系统(36),数据库(32)和处理器(22)。 数据库包括地形数据,机场数据,障碍物数据和受保护的空域数据。 处理器基于存储在数据库中的数据和从位置信息系统接收到的信息来确定是否存在警告警报之一。 如果在等待期满后没有执行正面飞行控制输入,则自动恢复指令被生成并发送到自动飞行控制系统。 基于两个或多个自动恢复路由的分析生成自动恢复指令。 如果系统的组件不能满足预定义的有效性或完整性级别,则系统不执行自动恢复。