Apparatus, method, and computer program product for generating terrain clearance floor envelopes about a selected runway
    51.
    发明授权
    Apparatus, method, and computer program product for generating terrain clearance floor envelopes about a selected runway 有权
    装置,方法和计算机程序产品,用于在所选择的跑道上产生地形清除地面信封

    公开(公告)号:US06707394B2

    公开(公告)日:2004-03-16

    申请号:US09496296

    申请日:2000-02-01

    IPC分类号: G08B2300

    CPC分类号: G05D1/0676 G01C5/005

    摘要: The present invention provides several apparatus, methods, and computer program products for generating a terrain clearance floor envelope for use in a ground proximity warning system. In one embodiment, the present invention includes a processor that defines a terrain clearance floor envelope having at least two boundaries. In this embodiment, the processor defines at least one of the boundaries based on a runway position quality factor, an altitude data quality factor, and an aircraft position quality factor. Using these factors, the processor of the present invention can more precisely define the boundaries of the envelope about the selected runway. Further, the processor of the present invention does not unnecessarily increase the region between the envelope and runway where no ground proximity alarms are generated. In another embodiment, the present invention includes a processor that defines the terrain clearance floor envelope to be asymmetrical, such that respective profiles of the envelope in a radial cross-section are different in at least two radial directions from a center point of the selected runway. Importantly, in one embodiment of the present invention, the processor defines end regions of the terrain clearance floor envelope adjacent to the ends of the selected runway to have a different slope profile than side regions of the terrain clearance floor envelope adjacent to the sides of the selected runway. This, in turn, allows the processor to define the end regions to reflect a landing pattern for an aircraft approaching the end of the selected runway, while also defining the side regions to reflect a flight pattern for an aircraft approaching the side of the selected runway.

    摘要翻译: 本发明提供了用于产生用于地面接近警告系统中的地形间隙地面信封的几种装置,方法和计算机程序产品。 在一个实施例中,本发明包括限定具有至少两个边界的地形间隙地面包层的处理器。 在该实施例中,处理器基于跑道位置质量因子,高度数据质量因子和飞机位置质量因子来定义至少一个边界。 使用这些因素,本发明的处理器可以更精确地定义关于所选跑道的信封的边界。 此外,本发明的处理器不会不必要地增加不产生接地接近警报的信封和跑道之间的区域。 在另一个实施例中,本发明包括一个处理器,该处理器将地形间隙底面信封定义为不对称的,使得在径向横截面中的包络的相应轮廓在从所选择的跑道的中心点起的至少两个径向方向上是不同的 。 重要的是,在本发明的一个实施例中,处理器限定与所选择的跑道的端部相邻的地形间隙地板信封的端部区域,以具有与邻近所述跑道侧面的地形间隙地板信封的侧部区域不同的斜率分布 选择跑道。 这反过来又允许处理器定义端部区域以反映接近所选跑道端部的飞行器的着陆模式,同时还限定侧面区域以反映接近所选跑道侧面的飞行器的飞行模式 。

    Solid-state image device with resin lens and resin contact layer
    52.
    发明授权
    Solid-state image device with resin lens and resin contact layer 失效
    具有树脂透镜和树脂接触层的固态成像装置

    公开(公告)号:US4667092A

    公开(公告)日:1987-05-19

    申请号:US564403

    申请日:1983-12-22

    申请人: Yasuo Ishihara

    发明人: Yasuo Ishihara

    CPC分类号: H01L31/0232 H01L31/02162

    摘要: In a solid-state image device comprising an image storage block having a block surface, a plurality of storage elements are embeded along the block surface to store an image in the form of electric charge. An overlying layer is deposited to form an array of optical lenses in correspondence to the storage elements. An intermediate layer is laid between the block surface and the overlying layer. Incident light focuses through the lenses and the intermediate layer onto the storage elements. The intermediate layer serves as an adjusting layer for adjusting a focal length.

    摘要翻译: 在包括具有块表面的图像存储块的固态图像装置中,沿着块表面嵌入多个存储元件以以电荷的形式存储图像。 沉积覆盖层以形成对应于存储元件的光学透镜阵列。 中间层铺设在块表面和上覆层之间。 入射光通过透镜和中间层聚焦到存储元件上。 中间层用作调整焦距的调整层。

    Solid-state imaging device having a reduced image lag
    53.
    发明授权
    Solid-state imaging device having a reduced image lag 失效
    具有减小的图像滞后的固态成像装置

    公开(公告)号:US4484210A

    公开(公告)日:1984-11-20

    申请号:US297759

    申请日:1981-08-31

    CPC分类号: H01L27/14831

    摘要: A solid-state imaging device has a semiconductor substrate of one conductive type. A plurality of light-charge converter regions, of the opposite conductivity type, are formed in the semiconductor substrate. A charge-voltage converter region, formed in the semiconductor substrate, converts the electric charge produced by the light-charge converter regions into a voltage. At least one charge transfer section is formed in the semiconductor substrate for transferring the electric charge produced by the light-charge converter regions to the charge-voltage converter region. At least one charge transfer gate section is in the semiconductor substrate and has a gate electrode for controlling the timing of a transfer of the electric charges from the light-charge converter regions to the charge transfer section. Pulses are generated with a predetermined pulse potential and applied to the gate electrode in the charge transfer gate section. The predetermined pulse potential has the relationshipV.sub.B +2.phi..sub.FP

    摘要翻译: 固态成像装置具有一种导电类型的半导体衬底。 在半导体衬底中形成有相反导电类型的多个光电荷转换器区域。 形成在半导体基板中的电荷 - 电压转换器区域将由光电荷转换器区域产生的电荷转换为电压。 在半导体衬底中形成至少一个电荷转移部分,用于将由光电荷转换器区域产生的电荷转移到电荷 - 电压转换器区域。 至少一个电荷转移栅极部分在半导体衬底中并且具有用于控制电荷从光电荷转换器区域转移到电荷转移部分的定时的栅电极。 产生具有预定脉冲电位的脉冲并施加到电荷转移栅极部分中的栅电极。 预定脉冲电位具有关系VB + 2 phi FP

    Two-dimensional charge-coupled device for high-resolution image pickup
and the like
    54.
    发明授权
    Two-dimensional charge-coupled device for high-resolution image pickup and the like 失效
    用于高分辨率图像拾取的二维电荷耦合器件等

    公开(公告)号:US4127877A

    公开(公告)日:1978-11-28

    申请号:US618416

    申请日:1975-10-01

    CPC分类号: H04N3/1575

    摘要: A two-dimensional charge-coupled device for relatively high resolution image pick up includes an imaging area, a storage area, and plural output registers for developing plural video signals delayed by predetermined intervals, e.g., integral multiples of one horizontal line trace period. The several register output signals are combined to provide a composite video signal characterized by a greater resolution vis-a-vis the direct CCD output.

    摘要翻译: 用于相对高分辨率图像拾取的二维电荷耦合器件包括成像区域,存储区域和用于显影以预定间隔延迟的多个视频信号的多个输出寄存器,例如一个水平线迹线周期的整数倍。 多个寄存器输出信号被组合以提供特征在于相对于直接CCD输出更大分辨率的复合视频信号。

    Systems and methods for adjusting target approach speed
    55.
    发明授权
    Systems and methods for adjusting target approach speed 有权
    调整目标进近速度的系统和方法

    公开(公告)号:US08996204B2

    公开(公告)日:2015-03-31

    申请号:US12821445

    申请日:2010-06-23

    IPC分类号: G05D1/00 G05D1/06

    摘要: Systems and methods for adjusting target approach speed for use in a “Too Fast” approach to landing condition. An exemplary system stores predefined maximum wind setting and a predefined reference speed and a pilot set bug speed value. A processing device sets a target speed equal to the bug speed, if the bug speed is less than the reference speed plus a value associated with a predefined maximum wind setting, and sets the target speed equal to the reference speed plus the max wind added value, if the manual bug speed is not less than the reference speed plus the max wind added value. An output device outputs an alert if the received aircraft speed is greater than the set target speed plus a predefined error value when the received aircraft location is within a threshold value of a touchdown point.

    摘要翻译: 调整目标进近速度的系统和方法用于“太快”的着陆条件。 示例性系统存储预定义的最大风力设定和预定的参考速度和飞行员设置的错误速度值。 如果错误速度小于参考速度加上与预定义的最大风力设定相关联的值,则处理设备将目标速度设置为等于故障速度,并将目标速度设置为等于参考速度加上最大风力附加值 ,如果手动的错误速度不低于参考速度加上最大风量附加值。 如果所接收的飞行器位置在接地点的阈值内,则所接收到的飞行器速度大于设定的目标速度加上预定义的误差值,则输出设备输出报警。

    SYSTEMS AND METHODS FOR MONITORING LOW SPEED OF A ROTORCRAFT
    56.
    发明申请
    SYSTEMS AND METHODS FOR MONITORING LOW SPEED OF A ROTORCRAFT 审中-公开
    用于监测转子低速的系统和方法

    公开(公告)号:US20140052314A1

    公开(公告)日:2014-02-20

    申请号:US13585276

    申请日:2012-08-14

    IPC分类号: G08B31/00 B64D43/02

    CPC分类号: B64D43/02

    摘要: Systems and methods to provide alerts when a rotorcraft is in a low airspeed condition. During takeoff or go-around, an aural alert is provided to the pilot before the aircraft slows to less than the effective translational lift speed. The aural, visual, and/or tactile alert gets the pilot's attention to manage the aircraft's airspeed before it is too late in this critical flight phase.

    摘要翻译: 当旋翼航空器处于低空速条件时提供警报的系统和方法。 在起飞或复飞期间,在飞机减速到小于有效平移提升速度之前,向飞行员提供听觉警报。 听觉,视觉和/或触觉警报使飞行员注意在这个关键飞行阶段太晚之前管理飞机的空速。

    SYSTEMS AND METHODS FOR PERFORMING EXCESSIVE NEGATIVE PITCH ALERT AND BIASING SINK RATE ALERT
    57.
    发明申请
    SYSTEMS AND METHODS FOR PERFORMING EXCESSIVE NEGATIVE PITCH ALERT AND BIASING SINK RATE ALERT 有权
    用于执行过大的负面提示警报和偏移波长提醒的系统和方法

    公开(公告)号:US20110276200A1

    公开(公告)日:2011-11-10

    申请号:US12821591

    申请日:2010-06-23

    IPC分类号: G05D1/08

    CPC分类号: G05D1/0858 G01C23/00

    摘要: Systems and methods that alert the pilot of the unusual negative pitch attitude. Additionally, the system can bias a “sink rate” envelope toward a more sensitive direction, such that the pilot can be alerted while (or before) a large sink rate is built up during an unusual negative pitch attitude condition.

    摘要翻译: 系统和方法提醒飞行员异常负俯仰姿态。 此外,系统可以将“下沉速率”信号偏向更敏感的方向,使得可以在(或之前)在异常负俯仰姿态条件期间建立大的下沉速率时警告飞行员。

    SYSTEM FOR MONITORING RNP FOR SAFE TERRAIN CLEARANCE
    58.
    发明申请
    SYSTEM FOR MONITORING RNP FOR SAFE TERRAIN CLEARANCE 有权
    监测RNP的安全地雷达清除系统

    公开(公告)号:US20100010694A1

    公开(公告)日:2010-01-14

    申请号:US11383532

    申请日:2006-05-16

    IPC分类号: G06F7/00 G08B23/00

    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。

    TAILWIND ALERTING SYSTEM TO PREVENT RUNWAY OVERRUNS
    59.
    发明申请
    TAILWIND ALERTING SYSTEM TO PREVENT RUNWAY OVERRUNS 有权
    TAILWIND报警系统,以防止RUNWAY OVERRUNS

    公开(公告)号:US20050270180A1

    公开(公告)日:2005-12-08

    申请号:US11161368

    申请日:2005-08-01

    IPC分类号: G01C5/00 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,并且启动顺风警报。