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    • 1. 发明授权
    • Systems and methods for handling the display and receipt of aircraft control information
    • 处理飞机控制信息的显示和接收的系统和方法
    • US08290643B2
    • 2012-10-16
    • US13252369
    • 2011-10-04
    • Sherwin S. ChenPeter D. GunnJohn Wiedemann
    • Sherwin S. ChenPeter D. GunnJohn Wiedemann
    • G06F19/00
    • G01C23/00
    • Methods and systems for handling aircraft control information are disclosed. A system in accordance with one embodiment of the invention includes a display medium coupleable to a flight manager, with the flight manager configured to receive and direct instructions for automatically controlling aircraft functions at a future time during flight of the aircraft. The system can further include a display controller coupled to the display medium to present at least one operator activatable element at the display medium and update information presented at the display medium when the operator activates the operator activatable element. For example, the operator activatable element can include an icon presented at a computer display screen, and can be activated by a keystroke.
    • 公开了处理飞机控制信息的方法和系统。 根据本发明的一个实施例的系统包括可与飞行管理器相连的显示介质,飞行管理器被配置为接收并指示在飞行器飞行期间将来的时间自动控制飞机功能的指令。 该系统还可以包括耦合到显示介质的显示控制器,以在操作员激活操作员可激活元件时,在显示介质上呈现至少一个操作员可激活元件,并更新呈现在显示介质上的信息。 例如,操作员可激活元件可以包括呈现在计算机显示屏幕处的图标,并且可以通过按键来激活。
    • 2. 发明授权
    • Automatic strategic offset function
    • 自动战略偏移功能
    • US08185258B2
    • 2012-05-22
    • US12713629
    • 2010-02-26
    • Michael E. DeyBradley D. CornellPeter D. GunnRobert J. Myers
    • Michael E. DeyBradley D. CornellPeter D. GunnRobert J. Myers
    • G01C23/00
    • G08G5/0052G08G5/0034
    • A system may generate a modified flight plan for an aircraft based on an original flight plan. The system may provide an automatic strategic offset function that includes an autoflight system; a sensor system including at least one of a global positioning system, an inertial reference unit, or an air data computer; and a flight management computer. The flight management computer may be operably coupled with the autoflight system and/or the sensor system. The flight management computer may process a flight plan of the vehicle and generate a non-uniform offset value in the vertical and/or lateral orientation between the flight plan and a boundary. The offset value may be used to create an offset flight plan for navigating an aircraft.
    • 系统可以根据原始飞行计划为飞机生成修改的飞行计划。 该系统可以提供包括自动飞行系统的自动战略偏移功能; 传感器系统,包括全球定位系统,惯性参考单元或空中数据计算机中的至少一个; 和飞行管理计算机。 飞行管理计算机可以与自动飞行系统和/或传感器系统可操作地耦合。 飞行管理计算机可以处理车辆的飞行计划,并且在飞行计划和边界之间的垂直和/或横向方向上产生不均匀的偏移值。 偏移值可用于创建用于航行飞机的偏移飞行计划。
    • 5. 发明授权
    • Systems and methods for handling the display and receipt of aircraft control information
    • 处理飞机控制信息的显示和接收的系统和方法
    • US07418319B2
    • 2008-08-26
    • US10814369
    • 2004-03-31
    • Sherwin S. ChenPeter D. GunnJohn Wiedemann
    • Sherwin S. ChenPeter D. GunnJohn Wiedemann
    • G05D1/00
    • G01C23/00
    • Methods and systems for handling aircraft control information are disclosed. A system in accordance with one embodiment of the invention includes a display medium coupleable to a flight manager, with the flight manager configured to receive and direct instructions for automatically controlling aircraft functions at a future time during flight of the aircraft. The system can further include a display controller coupled to the display medium to present at least one operator activatable element at the display medium and update information presented at the display medium when the operator activates the operator activatable element. For example, the operator activatable element can include an icon presented at a computer display screen, and can be activated by a keystroke.
    • 公开了处理飞机控制信息的方法和系统。 根据本发明的一个实施例的系统包括可与飞行管理器相连的显示介质,飞行管理器被配置为接收并指示在飞行器飞行期间将来的时间自动控制飞机功能的指令。 该系统还可以包括耦合到显示介质的显示控制器,以在操作员激活操作员可激活元件时,在显示介质上呈现至少一个操作员可激活元件,并更新呈现在显示介质上的信息。 例如,操作员可激活元件可以包括呈现在计算机显示屏幕处的图标,并且可以通过按键来激活。
    • 6. 发明授权
    • Apparatuses and methods for displaying and receiving tactical and strategic flight guidance information
    • 显示和接收战术和战略飞行指导信息的装置和方法
    • US07188007B2
    • 2007-03-06
    • US10746912
    • 2003-12-24
    • Daniel J. BoormanJohn C. Griffin, IIIPeter D. GunnRandall J. Mumaw
    • Daniel J. BoormanJohn C. Griffin, IIIPeter D. GunnRandall J. Mumaw
    • B64C23/00
    • G08G5/0021G01C23/00G08G5/0052
    • Methods and apparatuses for displaying and receiving tactical and strategic flight guidance information. A method in accordance with one aspect of the invention includes displaying at least one first indicator to an operator of the aircraft, with a first indicator corresponding to a first instruction input by the operator for directing a first aircraft behavior and implemented upon receiving an activation instruction from the operator. At least one second indicator corresponding to a second instruction for directing a second aircraft behavior at least proximately the same as the first aircraft behavior is displayed, with the at least one second instruction to be automatically implemented at a future time. The at least one second indicator is at least approximately the same as the at least one first indicator. Indicators can be hierarchically organized to simplify presentation and reduce pilot training time.
    • 展示和接收战术和战略飞行指导信息的方法和装置。 根据本发明的一个方面的方法包括将至少一个第一指示符显示给飞行器的操作者,其中第一指示符对应于由操作者输入的用于指示第一飞行器行为并在接收到激活指令时实现的第一指令 从运营商。 显示对应于用于将第二飞行器行为至少接近地与第一飞行器行为相同的第二指令的至少一个第二指示符,其中至少一个第二指令将在将来的时间自动实现。 所述至少一个第二指示器至少与所述至少一个第一指示器大致相同。 指标可以分层组织,以简化​​演示,减少飞行员培训时间。
    • 10. 发明授权
    • Apparatuses and systems for controlling autoflight systems
    • 用于控制自动曝光系统的设备和系统
    • US07970502B2
    • 2011-06-28
    • US12414559
    • 2009-03-30
    • Daniel J. BoormanPeter D. GunnJohn C. Griffin, III
    • Daniel J. BoormanPeter D. GunnJohn C. Griffin, III
    • G01C23/00
    • G01C23/00
    • Apparatuses and methods for controlling autoflight systems are disclosed herein. An apparatus for use with an aircraft having an autoflight system can include an autoflight performance selector configured to limit the response of the autoflight system to flight guidance instructions in at least two of the pitch, roll and yaw axes. The autoflight performance selector has at least a first selection and a second selection different than the first selection. Selecting the first selection causes the response of the autoflight system to flight guidance instructions to not exceed a first level in the at least two axes, and selecting the second selection causes the response of the autoflight system to the flight guidance instructions to not exceed a second level in the at least two axes different than the first level.
    • 本文公开了用于控制自动曝光系统的装置和方法。 一种与具有自动曝光系统的飞行器一起使用的装置可以包括自动飞行性能选择器,其被配置为将自动飞行系统的响应限制在俯仰,滚动和偏航轴中的至少两个中的飞行指导指令。 自动播放性能选择器至少具有与第一选择不同的第一选择和第二选择。 选择第一选择导致自动飞行系统对飞行指导指令的响应不超过至少两个轴上的第一级,并且选择第二选择导致自动飞行系统对飞行指导指令的响应不超过第二级 在至少两个不同于第一级的轴上的水平。