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    Method and apparatus for improving pilot situational awareness during flare to touchdown
    13.
    发明授权
    Method and apparatus for improving pilot situational awareness during flare to touchdown 有权
    改善飞弹状态感知的方法和装置

    公开(公告)号：US08126600B2

    公开(公告)日：2012-02-28

    申请号：US12141816

    申请日：2008-06-18

    申请人： Kevin J Conner ,  Yasuo Ishihara

    发明人： Kevin J Conner ,  Yasuo Ishihara

    IPC分类号： G06F19/00

    CPC分类号： G08G5/02

    摘要： A system and method for selectively alerting a pilot of an aircraft about distance remaining to the end of a runway. A position of the aircraft is received. A position of a runway is retrieved from a runway database. The retrieved position of the runway is compared to the received position of the aircraft to determine if the aircraft is within an alert envelope relative to the retrieved position of the runway. The position of the runway is subtracted from the position of the aircraft to determine a distance to the distal end of the runway. An alert to the pilot is generated based upon the distance to the distal end of the runway.

    摘要翻译： 一种系统和方法，用于选择性地提醒飞机的飞行员关于剩余到跑道末端的距离。 接收到飞机的位置。 从跑道数据库中检索跑道的位置。 将跑道的检索位置与飞机的接收位置进行比较，以确定飞机是否在相对于跑道的检索位置的警报信封内。 从飞机的位置减去跑道的位置，以确定到跑道远端的距离。 基于到跑道远端的距离产生对飞行员的警报。

    Systems and methods for detecting and alerting mis-setting of barometric altimeter setting during a transition altitude
    14.
    发明授权
    Systems and methods for detecting and alerting mis-setting of barometric altimeter setting during a transition altitude 有权
    在过渡高度期间检测和警报气压高度计设置错误设置的系统和方法

    公开(公告)号：US07778745B2

    公开(公告)日：2010-08-17

    申请号：US11469372

    申请日：2006-08-31

    申请人： Kevin J Conner ,  Yasuo Ishihara ,  Steve C. Johnson

    发明人： Kevin J Conner ,  Yasuo Ishihara ,  Steve C. Johnson

    IPC分类号： G01S1/00

    CPC分类号： G01C5/06

    摘要： Systems and methods for producing an advisory if barometric altitude transition setting needs adjusting in an aircraft. In one embodiment, the method determines transition altitude, receives an uncorrected altitude, compares the uncorrected altitude to the transition altitude and to corrected altitude, and outputs a barometric altitude transition setting advisory based on the comparison between the uncorrected altitude and the transition altitude. The comparison determines if the uncorrected altitude is greater than the determined transition altitude and the advisory is output if the uncorrected altitude is determined to be greater than the transition altitude and the uncorrected altitude differs from the corrected altitude by a threshold amount. A delay is provided between the comparison of the uncorrected altitude to the transition altitude and the comparison between the uncorrected altitude and the corrected altitude.

    摘要翻译： 生产咨询的系统和方法，如果气压高度转换设置需要在飞机上进行调整。 在一个实施例中，该方法确定过渡高度，接收未校正的高度，将未校正的高度与过渡高度和校正的高度进行比较，并且基于未校正的高度和过渡高度之间的比较输出气压高度转换设置咨询。 该比较确定未校正的高度是否大于所确定的过渡高度，并且如果未校正的高度被确定为大于过渡高度并且未校正的高度与校正的高度不同阈值量则输出咨询。 在未校正的高度与过渡高度的比较和未校正的高度与校正的高度之间的比较之间提供延迟。

    SYSTEMS AND METHODS FOR IMPROVING PILOT SITUATIONAL AWARENESS DURING LANDING
    16.
    发明申请
    SYSTEMS AND METHODS FOR IMPROVING PILOT SITUATIONAL AWARENESS DURING LANDING 审中-公开
    用于改善陆地期间导弹状态意识的系统和方法

    公开(公告)号：US20100036550A1

    公开(公告)日：2010-02-11

    申请号：US12186386

    申请日：2008-08-05

    申请人： Kevin J Conner ,  Yasuo Ishihara ,  C. Don Bateman

    发明人： Kevin J Conner ,  Yasuo Ishihara ,  C. Don Bateman

    IPC分类号： G05D1/00

    CPC分类号： B64D45/04

    摘要： Systems and methods for generating an alert to the pilot of an aircraft during a deep/long landing situation. An example system includes a database that stores runway information, a position sensor that produces aircraft position information and a processor that is in data communication with the database and the position sensor. The processor includes an advisory condition detection component that compares altitude of the aircraft to a predefined altitude limit, determines if the aircraft is beyond an airline defined landing zone limit and not on the ground, and generates an alert to the pilot based upon the comparison and the determination. An output device outputs the generated alert. The airline defined landing zone limit is a fixed distance value from the approach end of a runway or a percentage of the total length of a runway, whichever allows for greatest amount of runway remaining.

    摘要翻译： 在深/长着陆情况下，向飞机飞行员生成警报的系统和方法。 示例性系统包括存储跑道信息的数据库，产生飞行员位置信息的位置传感器和与数据库和位置传感器进行数据通信的处理器。 所述处理器包括将所述飞行器的高度与预定义的高度极限进行比较的建议条件检测部件，确定所述飞行器是否超出航空公司限定的着陆区域限制而不是在地面上，并且基于所述比较并且向所述飞行员生成警报， 决心。 输出设备输出生成的警报。 航空公司定义的着陆区域限制是距跑道接近端的固定距离值或跑道总长度的百分比，以允许最大跑道数量为准。

    SYSTEMS AND METHODS FOR DETECTING AND ALERTING MIS-SETTING OF BAROMETRIC ALTIMETER SETTING DURING A TRANSITION ALTITUDE
    18.
    发明申请
    SYSTEMS AND METHODS FOR DETECTING AND ALERTING MIS-SETTING OF BAROMETRIC ALTIMETER SETTING DURING A TRANSITION ALTITUDE 有权
    用于检测和报警过程中测量和设定BAROMETRIC ALTIMETER设定的系统和方法

    公开(公告)号：US20080059008A1

    公开(公告)日：2008-03-06

    申请号：US11469372

    申请日：2006-08-31

    申请人： Kevin J Conner ,  Yasuo Ishihara ,  Steve C. Johnson

    发明人： Kevin J Conner ,  Yasuo Ishihara ,  Steve C. Johnson

    IPC分类号： G01C5/00

    CPC分类号： G01C5/06

    摘要： Systems and methods for producing an advisory if barometric altitude transition setting needs adjusting in an aircraft. In one embodiment, the method determines transition altitude, receives an uncorrected altitude, compares the uncorrected altitude to the transition altitude and to corrected altitude, and outputs a barometric altitude transition setting advisory based on the comparison between the uncorrected altitude and the transition altitude. The comparison determines if the uncorrected altitude is greater than the determined transition altitude and the advisory is output if the uncorrected altitude is determined to be greater than the transition altitude and the uncorrected altitude differs from the corrected altitude by a threshold amount. A delay is provided between the comparison of the uncorrected altitude to the transition altitude and the comparison between the uncorrected altitude and the corrected altitude.

    摘要翻译： 生产咨询的系统和方法，如果气压高度转换设置需要在飞机上进行调整。 在一个实施例中，该方法确定过渡高度，接收未校正的高度，将未校正的高度与过渡高度和校正的高度进行比较，并且基于未校正的高度和过渡高度之间的比较输出气压高度转换设置咨询。 该比较确定未校正的高度是否大于所确定的过渡高度，并且如果未校正的高度被确定为大于过渡高度并且未校正的高度与校正的高度不同阈值量，则输出咨询。 在未校正的高度与过渡高度的比较和未校正的高度与校正的高度之间的比较之间提供延迟。

    SYSTEMS AND METHODS FOR INTELLIGENT ALERTING FOR CABIN ALTITUDE DEPRESSURIZATION
    19.
    发明申请
    SYSTEMS AND METHODS FOR INTELLIGENT ALERTING FOR CABIN ALTITUDE DEPRESSURIZATION 有权
    用于智能警报用于客舱高度减少的系统和方法

    公开(公告)号：US20080057849A1

    公开(公告)日：2008-03-06

    申请号：US11469376

    申请日：2006-08-31

    申请人： Kevin J. Conner ,  Yasuo Ishihara ,  Charles D. Bateman

    发明人： Kevin J. Conner ,  Yasuo Ishihara ,  Charles D. Bateman

    IPC分类号： B64D13/02 ,  B60H1/00

    CPC分类号： B64D13/02

    摘要： Methods and systems for providing a depressurization alert. An example method includes receiving a cabin depressurization discrete signal, determining if the cabin depressurization discrete signal is valid, and issuing a cabin depressurization alert, if the cabin depressurization discrete signal was determined to be valid. In accordance with further aspects of the invention, a time delay is executed before the receiving, determining, and issuing steps are repeated. The cabin depressurization discrete signal is determined not valid if uncorrected pressure is not greater than a predefined altitude. The uncorrected pressure is a raw pressure value produced by a Pitot-Static system. Also, the cabin depressurization discrete signal is determined not valid if the aircraft's altitude above an intended runway is not greater than a first predefined value. Additionally, the cabin depressurization discrete signal is determined not valid if an aircraft's altitude above terrain is not greater than a second predefined value.

    摘要翻译： 提供减压警报的方法和系统。 一种示例性方法包括：如果客舱减压离散信号被确定为有效，则接收客舱减压离散信号，确定客舱减压离散信号是否有效，并发出机舱减压警报。 根据本发明的其它方面，在重复接收，确定和发出步骤之前执行时间延迟。 如果未校正的压力不大于预定高度，则舱室减压离散信号被确定为无效。 未校正的压力是由皮托静力系统产生的原始压力值。 此外，如果飞机在预期跑道上方的高度不大于第一预定值，则机舱减压离散信号被确定为无效。 此外，如果飞机在地形上方的高度不大于第二预定义值，则机舱减压离散信号被确定为无效。

    System and method for using airport information based on flying environment
    20.
    发明授权
    System and method for using airport information based on flying environment 有权
    基于飞行环境使用机场信息的系统和方法

    公开(公告)号：US07133754B2

    公开(公告)日：2006-11-07

    申请号：US10703185

    申请日：2003-11-06

    申请人： Yasuo Ishihara ,  Steve C. Johnson ,  Kevin J Conner

    发明人： Yasuo Ishihara ,  Steve C. Johnson ,  Kevin J Conner

    IPC分类号： G06F19/00 ,  G06G7/70 ,  G01C5/00

    CPC分类号： G08G5/025 ,  G08G5/0065 ,  G08G5/0078

    摘要： A method, system, and computer program product for using airport information based on the flying environment are provided. When a helicopter is determined to be approaching a runway, ground proximity warning envelopes are automatically reduced to prevent unwanted, or nuisance, terrain alerts. On the other hand, when a helicopter is flown near a runway without intent to land or when a helicopter is taking off, ground proximity warning envelopes may remain unchanged. As a result, nuisance alerts are reduced when a helicopter is approaching a runway for landing and ground proximity warnings may remain in effect to maximize protection when a helicopter is flying near a runway without an intent to land or is taking off from a runway.

    摘要翻译： 提供了一种基于飞行环境使用机场信息的方法，系统和计算机程序产品。 当直升机决定接近跑道时，地面接近警告信封会自动降低，以防止不必要或令人讨厌的地形警报。 另一方面，当直升机在跑道附近没有意图着陆或直升机起飞时，地面接近警告信封可能保持不变。 因此，当直升机正在接近跑道进行着陆时，妨碍警报将减少，并且当直升机在跑道附近飞行而无意着陆或正在从跑道起飞时，地面邻近警报可能仍然有效，以最大限度地保护。