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    • 5. 发明申请
    • SELF-ADJUSTING SYSTEM FOR AIRCRAFT CONTROL
    • 航空器自动调整系统
    • WO2017218220A1
    • 2017-12-21
    • PCT/US2017/035824
    • 2017-06-02
    • KITTY HAWK CORPORATION
    • REICHERT, ToddVAWTER, ZachaisROOP, JosephCUTLER, Mark, Johnson
    • A63F9/24A63F13/00A63F13/12A63F13/20A63F13/98B60R21/00
    • A self-adjusting flight control system is disclosed. In various embodiments, an input interface receives an input signal generated by an inceptor based at least in part on a position of an input device comprising the inceptor. A processor coupled to the input interface determines dynamically a mapping to be used to map input signals received from the inceptor to corresponding output signals associated with flight control and uses the determined mapping to map the input signal to a corresponding output signal. The processor determines the mapping at least in part by computing a running average of the output signal over an averaging period and adjusting the mapping at least in part to associate a neutral position of the input device comprising the inceptor with a corresponding output level that is determined at least in part by the computed running average.
    • 公开了一种自调节飞行控制系统。 在各种实施例中,输入接口至少部分地基于包括感受器的输入装置的位置来接收由感测器生成的输入信号。 耦合到输入接口的处理器动态地确定要用于将从感测器接收的输入信号映射到与飞行控制相关联的对应输出信号的映射,并使用所确定的映射将输入信号映射到对应的输出信号。 处理器至少部分地通过在平均周期内计算输出信号的运行平均值并且至少部分地调整映射来确定映射,所述映射至少部分地将包括输入设备的输入设备的中性位置与被确定的对应输出水平相关联 至少部分取决于计算出的运行平均值。