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51. 发明授权

US09644990B2 Systems and methods for adjusting sink rate alert envelope for special landing zones 有权
公开(公告)号：US09644990B2
公开(公告)日：2017-05-09
申请号：US13286141
申请日：2011-10-31
申请人： Yasuo Ishihara , Steve Johnson , Gary A. Ostrom
发明人： Yasuo Ishihara , Steve Johnson , Gary A. Ostrom
IPC分类号： G08B23/00 , G01C23/00 , B64D45/04 , G01C21/00 , G05D1/06 , G08G5/00 , G08G5/02
CPC分类号： G01C23/00 , B64D45/04 , G01C21/00 , G05D1/0676 , G08G5/0021 , G08G5/0086 , G08G5/025
摘要： Systems and methods for improving sink rate alerting for rotary wing aircraft. In one example, the system includes a radio altimeter that produces an altitude value, a processor that is in signal communication with the user interface device and the radio altimeter. The processor receives an altitude value, a position value for the aircraft and landing zone (LZ) information. The processor determines if the aircraft is on an approach to land at an LZ that is raised above surrounding terrain based on the received position value and LZ information. The processor receives sink rate information for the aircraft and generates a sink rate alert based on the received sink rate information and the aircraft altitude value if the sink rate information is greater than a sink rate value adjusted according to the LZ information. An output device outputs the generated sink rate alert. The LZ information includes an altitude value.

52. 发明授权

US09426926B2 Secure flat wall mounting rack 有权
标题翻译：安全平板安装架
公开(公告)号：US09426926B2
公开(公告)日：2016-08-23
申请号：US14283516
申请日：2014-05-21
申请人： Sean Iwasaki , Jim Jay , Steve Johnson , Paul DeCraene
发明人： Sean Iwasaki , Jim Jay , Steve Johnson , Paul DeCraene
IPC分类号： H05K7/14 , H05K5/02 , H05K7/18 , H04Q1/02
CPC分类号： H05K7/186 , H04Q1/02 , H04Q1/09 , H05K5/0208 , H05K7/1498
摘要： A secure flat wall mounting rack for network service provider equipment and cabling is provided. The mounting rack not only restricts unauthorized access to network communication equipment, but is also properly labeled for authorized user. The rack is especially suitable for service demarcation applications involving patch panels. The flat wall mounting rack has a securing bar with a movable plate which, when extended, only allows authorized users to remove and/or access cabling connected to the service ports of an Ethernet service delivery switch. The securing bar also allows for securing service handoff modules to be secured to the same.
摘要翻译：提供了一种用于网络服务提供商设备和布线的安全平板安装架。安装架不仅限制了对网络通信设备的未经授权的访问，还为授权用户进行了正确的标记。该机架特别适用于涉及接线板的服务分界应用。平板安装架具有带有可移动板的固定杆，当延伸时，仅允许授权用户移除和/或接入连接到以太网服务交付交换机的服务端口的电缆。固定杆还允许将服务切换模块固定在其上。

53. 发明授权

US09261883B2 Systems and methods for performing excessive negative pitch alert and for biasing a sink rate alert 有权
标题翻译：用于执行过度负音高警报和偏置下沉速率警报的系统和方法
公开(公告)号：US09261883B2
公开(公告)日：2016-02-16
申请号：US12821591
申请日：2010-06-23
申请人： Yasuo Ishihara , Steve Johnson , Gary Ostrom
发明人： Yasuo Ishihara , Steve Johnson , Gary Ostrom
IPC分类号： G08B23/00 , G05D1/08 , G01C23/00
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。

54. 发明授权

US09134967B1 Method of providing interactive usage descriptions based on source code analysis 有权
标题翻译：基于源代码分析提供交互式使用说明的方法
公开(公告)号：US09134967B1
公开(公告)日：2015-09-15
申请号：US13283099
申请日：2011-10-27
申请人： Steve Johnson
发明人： Steve Johnson
IPC分类号： G06F9/44 , G06F9/45 , G06F3/00 , G06F11/36
CPC分类号： G06F8/33 , G06F8/427 , G06F8/436 , G06F8/437 , G06F11/3664
摘要： A method of dynamically analyzing source code for generating usage hints while editing the source code is disclosed. A parse tree data structure is generated for each function called. The incoming and outgoing arguments in the parse tree are identified. A user calls the function by entering arguments as part of the function-call. The user's input arguments are associated with the corresponding argument in the parse tree. Relevant preconditions and post-conditions of the nodes surrounding the current location in the parse tree are analyzed to provide usage hints for the completion of the function call. In the case of a completed function call argument entered by the user, the type and number of arguments in the completed function call are compared to the required type and number of arguments of the function to validate the function call. Error messages are provided in the event of an invalid call.
摘要翻译：公开了在编辑源代码时动态分析源代码以产生使用提示的方法。为每个调用的函数生成解析树数据结构。识别解析树中的传入和传出参数。用户通过输入参数作为函数调用的一部分来调用该函数。用户的输入参数与解析树中的相应参数相关联。分析围绕解析树中当前位置的节点的相关前提条件和后置条件，以提供完成函数调用的使用提示。在用户输入完成的函数调用参数的情况下，将完成函数调用中的参数的类型和数量与要验证函数调用的函数的必需类型和数量进行比较。在无效呼叫的情况下提供错误消息。

55. 发明申请

US20120095625A1 SYSTEMS AND METHODS FOR ALERTING POTENTIAL TAILSTRIKE DURING LANDING 有权
标题翻译：用于在着陆期间预警潜在的潜艇的系统和方法
公开(公告)号：US20120095625A1
公开(公告)日：2012-04-19
申请号：US12907392
申请日：2010-10-19
申请人： Yasuo Ishihara , Steve Johnson
发明人： Yasuo Ishihara , Steve Johnson
IPC分类号： G08B23/00
CPC分类号： B64D45/04 , B64C25/00 , B64D2045/008
摘要： Systems and methods for alerting for potential tailstrike during landing. A processing device located onboard an aircraft determines whether the aircraft is in a landing operational mode. If the aircraft is determined within the landing operational mode, the processing device determines whether aircraft speed is less than a previously defined threshold speed and generates an alert signal if it is determined that the aircraft's speed is less than the previously defined threshold speed. An output device located onboard the aircraft, outputs an alert based on the generated alert signal.
摘要翻译：用于在着陆期间潜在尾迹的警报的系统和方法。位于飞行器上的处理装置确定飞行器是否处于着陆操作模式。如果在着陆操作模式下确定飞行器，则处理装置确定飞行器速度是否小于先前定义的阈值速度，并且如果确定飞行器的速度小于先前定义的阈值速度，则产生报警信号。位于飞机上的输出设备基于生成的警报信号输出警报。

56. 发明申请

US20110273315A1 SYSTEMS AND METHODS FOR ADJUSTING LANDING GEAR ALERT ENVELOPE FOR OFFSHORE PLATFORMS AND BUILDING-TOP LANDINGS 有权
标题翻译：用于海上平台和建筑物起落架的调速齿轮报警装置的系统和方法
公开(公告)号：US20110273315A1
公开(公告)日：2011-11-10
申请号：US12821536
申请日：2010-06-23
申请人： Yasuo Ishihara , Steve Johnson , Gary Ostrom
发明人： Yasuo Ishihara , Steve Johnson , Gary Ostrom
IPC分类号： G08B23/00
CPC分类号： B64D45/0005
摘要： Systems and methods for improving landing gear alerting on a rotary wing aircraft. An example system includes a user interface device that allows a user to set a bug altitude value and a radio altimeter that produces an altitude value, both of which are in communication with a processor. The processor receives a bug altitude setting, generates a landing gear alert altitude value based on the received bug altitude setting and a predefined additive, receives a radio altitude value for the rotary-wing aircraft, and generates a landing gear alert if the radio altitude value is less than the landing gear alert altitude value and the landing gear is not in a landing position. An output device in signal communication with the processor, outputs the generated landing gear alert.
摘要翻译：用于改进旋翼机上起落架警报的系统和方法。示例性系统包括允许用户设置错误高度值的用户界面设备和产生高度值的无线电高度计，两者都与处理器通信。处理器接收到错误高度设置，根据接收到的臭虫高度设置和预定义的添加量生成起落架警报高度值，接收旋翼飞机的无线电高度值，并产生起落架警报，如果无线电高度值小于起落架报警高度值，起落架不在着陆位置。与处理器进行信号通信的输出设备输出生成的起落架警报。

57. 发明授权

US08051408B1 Method of providing interactive usage descriptions based on source code analysis 有权
标题翻译：基于源代码分析提供交互式使用说明的方法
公开(公告)号：US08051408B1
公开(公告)日：2011-11-01
申请号：US10940037
申请日：2004-09-13
申请人： Steve Johnson
发明人： Steve Johnson
IPC分类号： G06F9/44 , G06F9/45 , G06F3/00
CPC分类号： G06F8/33 , G06F8/427 , G06F8/436 , G06F8/437 , G06F11/3664
摘要： A method of dynamically analyzing source code to generate usage hints for a user performing program editing is disclosed. The functions in a collection of source code being edited by a user are processed so as to generate a parse tree data structure for each function called. The incoming and outgoing arguments in the parse tree are identified. Subsequently, a user editing code calls the function and either completely or incompletely enters the arguments as part of the function called. Input arguments are identified and associated with the corresponding argument in the parse tree for the function. Relevant preconditions and post-conditions of the surrounding nodes corresponding to the current location are analyzed. Usage hints are provided for the completion of the function call. Arguments for a completed function call argument entered by the user are validated. Error messages are delivered in the event of an invalid call.
摘要翻译：公开了一种动态分析源代码以为执行程序编辑的用户生成使用提示的方法。处理由用户编辑的源代码集合中的功能，以便为所调用的每个功能生成解析树数据结构。识别解析树中的传入和传出参数。随后，用户编辑代码调用该函数，并且完全或不完全地输入参数作为调用函数的一部分。输入参数被识别并与函数的解析树中的相应参数相关联。分析与当前位置对应的周围节点的相关前提条件和后置条件。提供了用于完成函数调用的提示。用户输入的已完成函数调用参数的参数将被验证。发生无效呼叫时发送错误消息。

58. 发明申请

US20110118911A1 STABILIZED APPROACH MONITOR 有权
标题翻译：稳定的方法监视器
公开(公告)号：US20110118911A1
公开(公告)日：2011-05-19
申请号：US12621794
申请日：2009-11-19
申请人： Yasuo Ishihara , Steve Johnson
发明人： Yasuo Ishihara , Steve Johnson
IPC分类号： G06F7/00
CPC分类号： G05D1/0676 , G08G5/0021 , G08G5/02 , G08G5/025
摘要： Systems and methods for suppressing an unstable alert when the aircraft is in the process of landing on a temporarily displaced threshold. In an example process, a processor on the aircraft determines the aircraft is on an approach to landing on a runway based on information received from one or more data sources on the aircraft, then retrieves predefined glideslope information for the runway from a memory device that is in signal communication with the processor. Next, the processor determines whether position of the aircraft is above the predefined glideslope by a first threshold amount. If the aircraft is determined to be above the predefined glideslope by the first threshold amount, the processor issues an unstable alert only if a flight path angle of the aircraft is greater than an angle of the predefined glideslope by a second threshold amount.
摘要翻译：当飞机正在临时移动的阈值上着陆的过程中用于抑制不稳定警报的系统和方法。在示例过程中，飞行器上的处理器基于从飞机上的一个或多个数据源接收到的信息来确定飞行器正在着陆在跑道上，然后从存储器设备中检索用于跑道的预定滑翔信息，与处理器进行信号通信。接下来，处理器确定飞行器的位置是否高于预定滑行边界第一阈值量。如果飞行器被确定为高于预定滑翔道第一阈值量，则只有当飞行器的飞行路径角度大于预定滑翔坡的角度达到第二阈值量时，处理器才发出不稳定的警报。

59. 发明申请

US20100145794A1 Media Processing Engine and Ad-Per-View 审中-公开
标题翻译：媒体处理引擎和Ad-Per-View
公开(公告)号：US20100145794A1
公开(公告)日：2010-06-10
申请号：US12489308
申请日：2009-06-22
申请人： Sean Barnes Barger , Steve Johnson , David Pochron , Jerry Destremps , Trent Brown
发明人： Sean Barnes Barger , Steve Johnson , David Pochron , Jerry Destremps , Trent Brown
IPC分类号： G06Q30/00 , G06F17/00 , G06Q10/00 , G06F17/30 , G06F3/01 , G06F15/16
CPC分类号： G06Q30/0254 , G06F16/9535 , G06F16/972 , G06Q30/0246
摘要： A scaleable server-based, on-demand media processing engine automates the production and delivery of media. A digital processing engine automatically transcodes a plurality of media files having different formats into a composite media file.
摘要翻译：可扩展的基于服务器的按需媒体处理引擎自动生成和传送媒体。数字处理引擎将具有不同格式的多个媒体文件自动转码为复合媒体文件。

60. 发明申请

US20070239326A1 Systems and methods for monitoring an altitude in a flight vehicle 审中-公开
标题翻译：用于监测飞行器高度的系统和方法
公开(公告)号：US20070239326A1
公开(公告)日：2007-10-11
申请号：US11398955
申请日：2006-04-05
申请人： Steve Johnson , Yasuo Ishihara , Charles Bateman
发明人： Steve Johnson , Yasuo Ishihara , Charles Bateman
IPC分类号： G01C23/00
CPC分类号： G01C5/06 , G08G5/0021 , G08G5/0052 , G08G5/0086
摘要： Systems and methods for monitoring an altitude in a flight vehicle are disclosed. In an embodiment, a system includes a barometric altimeter system operable to determine an altitude of the flight vehicle relative to a pressure datum that is adjustably selectable, and at least one altitude determination system that is operable to determine an altitude of the flight vehicle without reference to the selected pressure datum. A processor is coupled to the barometric altimeter system and to the at least one altitude determination system that is operable to receive altitude information from the barometric altimeter system and the at least one altitude determination system to compare the respective altitude information and determine if an altitude discrepancy exists.
摘要翻译：公开了用于监视飞行器中的高度的系统和方法。在一个实施例中，系统包括气压高度计系统，其可操作以相对于可调节地选择的压力数据来确定飞行车辆的高度;以及至少一个高度确定系统，其可操作以确定没有参考的飞行器的高度到选定的压力基准。处理器耦合到气压高度计系统和至少一个高度确定系统，其可操作以从气压高度计系统和至少一个高度确定系统接收高度信息，以比较相应的高度信息并确定高度差异存在

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