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    METHODS AND SYSTEMS FOR MONITORING APPROACH OF ROTARY WING AIRCRAFT
    11.
    发明申请
    METHODS AND SYSTEMS FOR MONITORING APPROACH OF ROTARY WING AIRCRAFT 审中-公开
    用于监控旋转飞机的方法和系统

    公开(公告)号：US20080173753A1

    公开(公告)日：2008-07-24

    申请号：US11625673

    申请日：2007-01-22

    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： B64D45/04

    CPC分类号： G05B23/0235

    摘要： Systems and methods for generating an alert if a rotary wing aircraft is approaching a hazardous situation. In an example method a processor receives a wind value and a rate of descent value. An alert signal is generated if the received wind value is greater than a tailwind threshold value and the rate of descent value is greater than a rate of descent threshold value. The generated alert is outputted to an output device, such as a display device or speakers. The alert signal is further generated if the rotary wing aircraft is on approach to landing, a rate of change of heading is less than a predefined value, or a rate of change in speed is less than a predefined value.

    摘要翻译： 如果旋翼飞机正在接近危险情况，产生警报的系统和方法。 在示例性方法中，处理器接收风值和下降速率值。 如果接收到的风值大于顺风阈值并且下降速率值大于下降阈值的速率，则产生报警信号。 生成的警报被输出到诸如显示装置或扬声器的输出装置。 如果旋转翼飞机正在着陆，则航向变化率小于预定值，或速度变化率小于预定值，进一步产生报警信号。

    Systems and methods for automatic detection of QFE operations
    12.
    发明授权
    Systems and methods for automatic detection of QFE operations 有权
    自动检测QFE操作的系统和方法

    公开(公告)号：US07389164B1

    公开(公告)日：2008-06-17

    申请号：US11625714

    申请日：2007-01-22

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

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

    IPC分类号： G01C5/00

    CPC分类号： G01C5/005

    摘要： Systems and methods for determining if an aircraft is approaching a atmospheric pressure at field elevation (QFE) airport and for alerting if any errors that might affect the production of an accurate altitude value. In an example method a global positioning system (GPS) altitude value is compared to a corrected barometric altitude, if an airport that the aircraft is proximate to (approaching) is a QFE airport. The field elevation of the proximate airport is added to the corrected barometric altitude to generate an adjusted barometric altitude, if the comparison between the GPS altitude and the corrected barometric altitude is greater than a predefined threshold. The adjusted barometric altitude is sent to relevant aircraft systems, such as an Enhanced Ground Proximity Warning System.

    摘要翻译： 用于确定飞机是否在场高程（QFE）机场接近大气压力的系统和方法，以及是否有可能影响准确高度值生产的错误的警报。 在示例性方法中，如果飞机靠近（接近）的机场是QFE机场，则将全球定位系统（GPS）高度值与校正的气压高度进行比较。 如果GPS高度与校正气压高度之间的比较大于预定义的阈值，则将邻近机场的场高程添加到校正的气压高度以产生调整的气压高度。 调整后的气压高度被发送到相关飞机系统，例如增强型地面接近警告系统。

    METHODS AND SYSTEMS FOR DISTINGUISHING ARINC 743 FROM ARINC 743A PROTOCOLS
    13.
    发明申请
    METHODS AND SYSTEMS FOR DISTINGUISHING ARINC 743 FROM ARINC 743A PROTOCOLS 有权
    从ARINC 743A协议中分离ARINC 743的方法和系统

    公开(公告)号：US20080068259A1

    公开(公告)日：2008-03-20

    申请号：US11469387

    申请日：2006-08-31

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

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

    IPC分类号： G01S5/14

    CPC分类号： G01S19/15 ,  G01S19/09 ,  G01S19/20 ,  G01S19/23

    摘要： An apparatus and method for automatically adjusting for data protocol discrepancies. The apparatus includes a unit that receives a signal from GPS receiver. The signal was formatted according to a transmission protocol. The unit includes a first component that estimates User Equivalent Range Error (UERE) based on the received signal and adjusting at least one value of the received signal based on the estimated UERE and one or more predefined scale factor and a second component that uses the adjusted at least one value.

    摘要翻译： 一种用于自动调整数据协议差异的装置和方法。 该装置包括从GPS接收器接收信号的单元。 信号根据传输协议格式化。 该单元包括基于接收到的信号来估计用户等效范围误差（UERE）的第一组件，并且基于估计的UERE和一个或多个预定比例因子调整接收信号的至少一个值，以及使用调整后的第二组件 至少有一个值。

    Automatic detection of GPS SA base value for HFOM
    15.
    发明授权
    Automatic detection of GPS SA base value for HFOM 有权
    自动检测HF SA的GPS SA基值

    公开(公告)号：US07570205B2

    公开(公告)日：2009-08-04

    申请号：US11161340

    申请日：2005-07-29

    申请人： Kevin J Conner ,  Steve C. Johnson

    发明人： Kevin J Conner ,  Steve C. Johnson

    IPC分类号： G01S1/00 ,  G01S5/14

    CPC分类号： G01S19/13 ,  G01S19/42

    摘要： An apparatus and method for detecting the type of Selective Availability (SA) engine in a Global Positioning System (GPS) receiver. The apparatus reverse computes a User Equivalent Range Error (UERE) value and filters it. The filtered value is run through a hysteresis to determine the GPS engine type. The engine type determination is used to adjust values used by other systems.

    摘要翻译： 一种用于在全球定位系统（GPS）接收机中检测选择性可用性（SA）引擎的类型的装置和方法。 设备反向计算用户等效范围误差（UERE）值并对其进行过滤。 滤波后的值通过滞后运行来确定GPS引擎类型。 引擎类型确定用于调整其他系统使用的值。

    SYSTEMS AND METHODS FOR SELECTIVELY ALTERING A GROUND PROXIMITY MESSAGE
    17.
    发明申请
    SYSTEMS AND METHODS FOR SELECTIVELY ALTERING A GROUND PROXIMITY MESSAGE 有权
    用于选择地面邻近信息的系统和方法

    公开(公告)号：US20100286851A1

    公开(公告)日：2010-11-11

    申请号：US12696555

    申请日：2010-01-29

    申请人： Yasuo Ishihara ,  Steve C. Johnson

    发明人： Yasuo Ishihara ,  Steve C. Johnson

    IPC分类号： G08G5/04

    CPC分类号： G01C23/005 ,  G08G5/0021 ,  G08G5/0086 ,  G08G5/045

    摘要： Systems and methods for selectively altering a ground proximity warning message. In an embodiment, a ground proximity warning system for a flight vehicle includes a processor that is configured to generate a look-ahead envelope that defines a region extending outwardly from the flight vehicle and to generate a terrain proximity message when the defined region intersects a terrain feature. An interface device is coupled to the processor that is operable to configure the system in a first operating mode wherein the generated terrain proximity message is selectively suppressed, and a second operating mode wherein the terrain proximity message is not suppressed.

    摘要翻译： 选择性地改变地面接近警告信息的系统和方法。 在一个实施例中，用于飞行器车辆的地面接近警告系统包括处理器，该处理器被配置为产生一个前视信封，该信号限定从飞行车辆向外延伸的区域，并且当定义的区域与地形相交时产生地形接近消息 特征。 接口设备耦合到处理器，其可操作以在第一操作模式中配置系统，其中选择性地抑制所生成的地形接近消息，以及其中不抑制地形接近消息的第二操作模式。

    System for monitoring RNP for safe terrain clearance
    18.
    发明授权
    System for monitoring RNP for safe terrain clearance 有权
    用于监测RNP的安全地形清除系统

    公开(公告)号：US07693618B2

    公开(公告)日：2010-04-06

    申请号：US11383532

    申请日：2006-05-16

    申请人： Steve C. Johnson ,  Yasuo Ishihara

    发明人： Steve C. Johnson ,  Yasuo Ishihara

    IPC分类号： G08G5/00

    CPC分类号： G01C23/005 ,  G08G5/0013 ,  G08G5/0021 ,  G08G5/0052 ,  G08G5/0078

    摘要： Systems and methods for monitoring Required Navigational Performance (RNP) Procedures and reducing nuisance Enhanced Ground Proximity Warning System warnings including a processor, a memory with RNP instructions and data, and a communication device. The processor accesses the RNP data and instructions from the memory, and uses the communication device to obtain flight information from a Flight Management System of an aircraft. When the processor determines that the aircraft is in RNP space, the processor projects an RNP envelope and modifies a warning envelope of an EGPWS to coincide with the RNP envelope if the EGPWS warning envelope extends farther than the RNP envelope.

    摘要翻译： 用于监测的系统和方法所需的导航性能（RNP）程序和减少滋扰增强的地面接近警告包括处理器，具有RNP指令和数据的存储器以及通信设备的系统警告。 处理器从存储器访问RNP数据和指令，并使用通信设备从飞行器的飞行管理系统获取飞行信息。 当处理器确定飞机处于RNP空间时，如果EGPWS警告信号比RNP信封更远，则处理器投射RNP信封并修改EGPWS的警告信号以与RNP信封一致。

    Glideslope monitor for aircraft
    19.
    发明授权
    Glideslope monitor for aircraft 失效

    公开(公告)号：US06600977B2

    公开(公告)日：2003-07-29

    申请号：US09916633

    申请日：2001-07-27

    申请人： Steve C. Johnson ,  Yasuo Ishihara

    发明人： Steve C. Johnson ,  Yasuo Ishihara

    IPC分类号： G08G500

    CPC分类号： G08G5/025 ,  G01C5/005 ,  G01S1/022 ,  G01S1/18 ,  G05D1/0676

    摘要： A system, method, and computer program product for alerting an aircraft flight crew of an inconsistency during an instrument landing system (ILS) approach to a selected runway. The system includes a component configured to receive glideslope and localizer signals, and a component configured to determine aircraft approach angle to runway end. Also, a component configured to alert the aircraft flight crew of an approach inconsistency, if the determined aircraft approach angle to runway end is less than a threshold angular value and one or more parameters based on aircraft position and the received glideslope and localizer signals are met. The component configured to determine aircraft approach angle to runway end determines the aircraft approach angle to runway end based on aircraft geometric altitude, a vertical figure of merit, a horizontal figure of merit, runway elevation, and aircraft distance to runway threshold.

    Tailwind alerting system to prevent runway overruns
    20.
    发明授权
    Tailwind alerting system to prevent runway overruns 有权
    尾风警报系统防止跑道超限

    公开(公告)号：US07394402B2

    公开(公告)日：2008-07-01

    申请号：US11161368

    申请日：2005-08-01

    申请人： Yasuo Ishihara ,  Steve C. Johnson

    发明人： Yasuo Ishihara ,  Steve C. Johnson

    IPC分类号： G08B23/00

    CPC分类号： G05D1/0676 ,  G01C5/005

    摘要： Systems, methods and computer program products for alerting a flight crew during landing that the tailwind exceeds acceptable limits. The system determines a base tailwind threshold speed for a candidate runway based on a performance constant associated with an aircraft and candidate runway information and determines present tailwind speed. If the tailwind speed is greater than the base tailwind threshold speed, a tailwind alert is generated. Also, the system determines if the aircraft is in a tailwind alerting mode based on configuration of the aircraft and activates tailwind alerting, if it is determined that the aircraft is in the tailwind alerting mode.

    摘要翻译： 系统，方法和计算机程序产品，用于在着陆期间提醒飞行机组人员，后排超过可接受的限制。 系统基于与飞行器和候选跑道信息相关联的性能常数来确定候选跑道的基本倒带阈值速度，并确定当前的顺风速度。 如果顺风速度大于基本的倒档门限速度，则会产生顺风警报。 此外，如果确定飞行器处于顺风警报模式，则系统基于飞行器的配置来确定飞行器是否处于顺风警报模式，并启动顺风警报。