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    • 1. 发明授权
    • Flight management system using holding pattern entry algorithms
    • 飞行管理系统采用保持模式进入算法
    • US07003383B2
    • 2006-02-21
    • US10439414
    • 2003-05-15
    • Jim R. RumboChad E. GaierJohn C. HadleyAdib BouananiGregory S. Hill
    • Jim R. RumboChad E. GaierJohn C. HadleyAdib BouananiGregory S. Hill
    • G05D1/00G06F17/00
    • G05D1/0202
    • The present invention provides a set of holding pattern entry algorithms used to define flight segments for entry into holding patterns. These geometries preferably describe the specific location and distance of various segments used in the holding pattern and holding pattern racetrack, with each segment defined as a curved or straight segment between endpoints. The algorithms also preferably include criteria used to determine entry extension, maximum initial turn angle, and minimum distance between a hold fix and an entry turn point. The geometry also preferably extends entry distance to avoid excessive iterative calculations. The algorithms are preferably utilized by a flight management system and method that determines segment sequencing during entry into holding patterns and the holding patterns themselves. The flight management system and method monitors the aircraft's progress along the active segment of the flight plan to determine what is the appropriate next segment in the algorithm and when to switch control from the active segment to the next segment.
    • 本发明提供一组用于定义用于进入保持模式的飞行段的保持模式输入算法。 这些几何形状优选地描述了在保持图案和保持图案跑道中使用的各种段的具体位置和距离,其中每个段被定义为端点之间的弯曲或直线段。 算法还优选地包括用于确定入口延伸,最大初始转角以及保持固定与入口转折点之间的最小距离的标准。 几何形状还优选地延伸进入距离以避免过度的迭代计算。 飞行管理系统和方法优选地利用这些算法,该飞行管理系统和方法在进入保持模式和保持模式本身期间确定段排序。 飞行管理系统和方法根据飞行计划的活动段监视飞机的进度,以确定算法中适当的下一段是什么,何时将控制从活动段切换到下一段。
    • 3. 发明授权
    • System and method for generating flyable paths for an aircraft
    • 用于为飞机生成可飞行路径的系统和方法
    • US07487039B2
    • 2009-02-03
    • US11506069
    • 2006-08-16
    • Jim R. RumboMichael R. SeastrandJames K. Haberstock
    • Jim R. RumboMichael R. SeastrandJames K. Haberstock
    • G01C21/34
    • G08G5/0034
    • A system and method are provided for generating a flight plan between an initial position and a destination. An input device is configured to receive inputs related to the destination; a memory configured to store data related to the destination; and a processor is configured to retrieve data from the memory and to generate the flight plan from the initial position to the destination. The flight plan includes a plurality of legs and an initial plurality of transitions between the legs. The processor is further configured to determine whether each of the initial plurality of transitions between the legs are flyable and to provide a flyable transition between the legs if the transition is not flyable.
    • 提供了一种用于在初始位置和目的地之间生成飞行计划的系统和方法。 输入设备被配置为接收与目的地相关的输入; 存储器,被配置为存储与所述目的地有关的数据; 并且处理器被配置为从存储器检索数据并且从初始位置到目的地生成飞行计划。 飞行计划包括多个腿和腿之间的初始多个过渡。 处理器还被配置为确定腿之间的初始多个转换中的每一个是否是可飞行的,并且如果转换不可飞行,则在腿之间提供可飞行转换。
    • 4. 发明授权
    • Aircraft control system for reaching a waypoint at a required time of arrival
    • 飞机控制系统,在达到所需的时间到达航点
    • US06507782B1
    • 2003-01-14
    • US09855861
    • 2001-05-14
    • Jim R. RumboMichael R. JacksonBrian E. O'Laughlin
    • Jim R. RumboMichael R. JacksonBrian E. O'Laughlin
    • G06F1550
    • G05D1/0202G05D1/0005
    • The instant invention provides a system and method for controlling the flight of an aircraft to meet an RTA. The system comprises a speed profile generator that communicates with a trajectory generator to produce a speed profile signal that enables the aircraft to reach a waypoint substantially at a predetermined time. In the system of the instant invention, the speed profile generator receives a nominal speed command signal, a time error signal and a sensitivity signal. Based on these inputs, the speed profile generator produces a speed profile signal. The trajectory generator receives the speed profile signal and a required time of arrival signal. Based on these signals, the trajectory generator produces a time error signal and a sensitivity signal. This sensitivity signal represents the sensitivity of the time error signal to changes in the speed profile signal.
    • 本发明提供了一种用于控制飞行器满足RTA的飞行的系统和方法。 该系统包括与轨迹发生器通信以产生速度分布信号的速度曲线发生器,该速度曲线信号使飞机能够在预定时间内达到航点。 在本发明的系统中,速度曲线发生器接收标称速度指令信号,时间误差信号和灵敏度信号。 基于这些输入,速度曲线生成器产生速度曲线信号。 轨迹发生器接收速度曲线信号和所需的到达时间信号。 基于这些信号,轨迹发生器产生时间误差信号和灵敏度信号。 该灵敏度信号表示时间误差信号对速度分布信号变化的灵敏度。