近地警告系统
1. 一种近地警告计算机检测系统
申请号: CN201920090127.5
申请日: 2019-01-18
公开（公告）号: CN209803778U
公开（公告）日: 2019-12-17
发明人: 杨硕; 王鹏; 牛鹏飞; 邱雪盼; 刘学军
本实用新型提供一种近地警告计算机检测系统，包括近地警告计算机、试验器和电脑，所述近地警告计算机包括：近地警告计算机本体，设置在近地警告计算机本体内的控制器和与控制器相连的ARINC-429数据总线，所述近地警告计算机本体外表面上设置有若干接口，所述接口位于近地警告计算机本体内部的一端与ARINC-429数据总线相连、所述接口位于近地警告计算机本体外部的一端与检测近地警告计算机的试验器相连，所述试验器与电脑相连。优点是：通过将ARINC-429数据总线引出，能够非常直观的通过电脑观察ARINC-429数据总线的输入输出情况，进而确定近地警告计算机中的故障点。
更多2. 一种基于卫星定位陆基增强的近地警告系统
申请号: CN202020876811.9
申请日: 2020-05-22
公开（公告）号: CN212410861U
公开（公告）日: 2021-01-26
发明人: 赵巍巍; 刘渡辉; 曹凯均; 蒋维安
本实用新型涉及一种基于卫星定位陆基增强的近地警告系统，包括GBAS差分定位器、近地警告计算机和报警器；所述近地警告计算机分别与所述GBAS差分定位器和所述报警器通信连接，所述GBAS差分定位器与卫星通信连接。本实用新型构成了一种新型的增强型近地告警系统，基于卫星定位陆基增强技术，有效改善了卫星计算的经纬度信息，大大提高了飞机导航数据的可靠性，从而大大增加了近地警告系统的告警精度和可靠性，有效提高了飞机的安全性。
更多3. 用于在地面以上和以下操作或在其间移动的人员、设备和装备的计算机化追踪和接近警告方法及系统
申请号: CN201480081546.2
申请日: 2014-09-10
公开（公告）号: CN107079259A
公开（公告）日: 2017-08-18
发明人: 珍妮特·琼斯
一种计算机化安全追踪和接近警告方法和系统，用于在地面以上和以下两者操作并在其间移动的人员、设备和装备，包括：适于经由一个或多个无线通信协议接收来自由所述人员携带或佩戴的和附加到设备或装备的应答器的无线位置信息的计算机，以在无论是在地平面以上还是以下或在其间移动时，提供它们相对位置的无缝视觉显示，并且其中如果人员和设备或装备的位置在预定的且不安全的彼此距离内，则触发报警器以警示操作者或工人。
更多4. 增强型近地警告系统的功能及故障的自动测试系统
申请号: CN201721190066.7
申请日: 2017-09-18
公开（公告）号: CN207232754U
公开（公告）日: 2018-04-13
发明人: 周卫稳; 杨保田
本实用新型涉及增强型近地警告系统的功能及故障的自动化测试系统，其包括嵌入式控制器、开关资源、多种测试设备以及测试接口适配器。嵌入式控制器运行有自动化测试软件平台与相应的测试脚本程序，控制待测的增强型近地警告系统、测试设备和测试接口适配器按照参数测试的流程完成功能和故障测试。测试设备包括函数信号发生器、数字万用表、可编程电源、示波器和计数器。开关资源将测试设备通过测试接口适配器连接到待测的增强型近地警告系统的测量点。测试接口适配器由自动化测试所需的电子元件及连接线组成，用于待测的增强型近地警告系统与测试设备之间的连接。本实用新型能够实现增强型近地警告系统的全自动化功能以及故障的测试。
更多5. GROUND PROXIMITY WARNING SYSTEM
申请号: EP96926212.0
申请日: 1996-07-31
公开（公告）号: EP0842396B1
公开（公告）日: 2004-09-22
发明人: MULLER, Hans, R.; CONNER, Kevin, J.; JOHNSON, Steven, C.
更多6. GROUND PROXIMITY WARNING SYSTEM
申请号: EP96926212.0
申请日: 1996-07-31
公开（公告）号: EP0842396A1
公开（公告）日: 1998-05-20
发明人: MULLER, Hans, R.; CONNER, Kevin, J.; JOHNSON, Steven, C.
A terrain awareness system (TAS) provides LOOK-AHEAD/LOOK-DOWN as well as LOOK-UP terrain advisory and warning indications to the pilot of an aircraft of a hazardous flight condition. The TAS includes an airport data base as well as a terrain data base that is structured to provide various resolutions depending on the topography of the particular geographic area of interest. Navigational data from a satellite-based navigational system, such as a global positioning system (GPS), is used to provide a LOOK-AHEAD/LOOK-DOWN and LOOK-UP terrain advisory and terrain warning indications based upon the current position and projected flight path of the aircraft. Since the terrain advisory and the warning signals are a function of the flight path of the aircraft, nuisance warnings are minimized.
更多7. 接近警報システム
申请号: JP2013101439
申请日: 2013-05-13
公开（公告）号: JP6093239B2
公开（公告）日: 2017-03-08
发明人: 澤田 喜久三; 原野 信也; 荒牧 佳秀; 佐藤 宙
更多8. GROUND PROXIMITY WARNING SYSTEM
申请号: EP00910044.7
申请日: 2000-02-01
公开（公告）号: EP1151244A1
公开（公告）日: 2001-11-07
发明人: CONNER, Kevin, J.; JOHNSON, Steven, C.
The present invention provides several apparatus, methods, and computer program products for determining a look ahead distance value for use in a ground proximity warning system. The apparatus, methods, and computer program products generate a candidate look ahead distance value that provides a constant reaction time for varying aircraft speeds. A processor generates the constant reaction time look ahead distance by multiplying a desired reaction time by the speed of the aircraft. This distance is compared by the processor to other candidate look ahead distance values that have variable reaction times for varying aircraft speeds. If the aircraft is traveling at a relatively high speed, the processor selects the constant reaction time look ahead distance value for use in the ground proximity warning system. The present invention can provide a look ahead distance value that reduces nuisance alarms for lower speeds, while also providing at least a minimum reaction time for higher speeds.
更多9. GROUND PROXIMITY WARNING SYSTEM
申请号: EP01959262.5
申请日: 2001-07-27
公开（公告）号: EP1354178B1
公开（公告）日: 2011-04-13
发明人: CONNER, Kevin; ISHIHARA, Yasuo; JOHNSON, Steven, C.
A terrain avoidance system, method and computer program product for reducing nuisance alarms. The system includes a geometric altitude component, first and second vertical safety margin generators, and an alert component.
更多10. TERRAIN AWARENESS SYSTEM
申请号: EP97941400.0
申请日: 1997-09-03
公开（公告）号: EP0925518A1
公开（公告）日: 1999-06-30
发明人: CONNER, Kevin, J.; MULLER, Hans, Rudolph
A terrain awareness system and method which provides increased warning times to the pilot of an aircraft of a hazardous flight condition while minimizing nuisance warnings. An important aspect of the invention is that the terrain background information as well as the terrain advisory and warning indications may be displayed on a navigational or weather display, normally existing within an aircraft, which reduces the cost of the system and obviates the need for extensive modifications to existing displays, such as a navigational and weather radar type display.
更多11. GROUND PROXIMITY WARNING SYSTEM
申请号: EP00910044.7
申请日: 2000-02-01
公开（公告）号: EP1151244B1
公开（公告）日: 2009-03-18
发明人: CONNER, Kevin, J.; JOHNSON, Steven, C.
The present invention provides several apparatus, methods, and computer program products for determining a look ahead distance value for use in a ground proximity warning system. The apparatus, methods, and computer program products generate a candidate look ahead distance value that provides a constant reaction time for varying aircraft speeds. A processor generates the constant reaction time look ahead distance by multiplying a desired reaction time by the speed of the aircraft. This distance is compared by the processor to other candidate look ahead distance values that have variable reaction times for varying aircraft speeds. If the aircraft is traveling at a relatively high speed, the processor selects the constant reaction time look ahead distance value for use in the ground proximity warning system. The present invention can provide a look ahead distance value that reduces nuisance alarms for lower speeds, while also providing at least a minimum reaction time for higher speeds.
更多12. TERRAIN AWARENESS SYSTEM
申请号: EP97941400.0
申请日: 1997-09-03
公开（公告）号: EP0925518B1
公开（公告）日: 2009-03-18
发明人: CONNER, Kevin, J.; MULLER, Hans, Rudolph
A terrain awareness system and method which provides increased warning times to the pilot of an aircraft of a hazardous flight condition while minimizing nuisance warnings. An important aspect of the invention is that the terrain background information as well as the terrain advisory and warning indications may be displayed on a navigational or weather display, normally existing within an aircraft, which reduces the cost of the system and obviates the need for extensive modifications to existing displays, such as a navigational and weather radar type display.
更多13. GROUND PROXIMITY WARNING SYSTEM
申请号: EP01959262.5
申请日: 2001-07-27
公开（公告）号: EP1354178A1
公开（公告）日: 2003-10-22
发明人: CONNER, Kevin; ISHIHARA, Yasuo; JOHNSON, Steven, C.
A terrain avoidance system, method and computer program product for reducing nuisance alarms. The system includes a geometric altitude component, first and second vertical safety margin generators, and an alert component.
更多15. GROUND PROXIMITY WARNING SYSTEM AND METHOD
申请号: EP03814370.7
申请日: 2003-12-22
公开（公告）号: EP1588228A2
公开（公告）日: 2005-10-26
发明人: REYNOLDS, Zachary; RIDENOUR, Richard; STONE, Cyro; ROWLAN, Stacey
Methods and systems are disclosed for preventing aircraft collisions with forward looking terrain avoidance (FLTA) functionality based on a terrain avoidance profile used to evaluate potential terrain threats based on the projected flight path of an aircraft in flight, and a clear terrain profile to determine whether the terrain threat has been cleared. If the terrain avoidance profile conflicts with terrain, a collision threat may exist whereby the pilot is notified and a terrain avoidance maneuver is executed. During the terrain avoidance maneuver the clear terrain profile extends in a direction substantially parallel with the horizon at or near the present altitude of the aircraft to check whether it is safe to return to the previous flight path angle or otherwise end the terrain-avoiding maneuver. When the clear terrain profile no longer conflicts with the terrain threat, a terrain clear indicator is then issued to the pilot.
更多16. GROUND PROXIMITY WARNING SYSTEM
申请号: PCT/US1996012561
申请日: 1996-07-31
公开（公告）号: WO1997005450A1
公开（公告）日: 1997-02-13
发明人: ALLIEDSIGNAL INC.; MULLER, Hans, R.; CONNER, Kevin, J.; JOHNSON, Steven, C.
A terrain awareness system (TAS) provides LOOK-AHEAD/LOOK-DOWN as well as LOOK-UP terrain advisory and warning indications to the pilot of an aircraft of a hazardous flight condition. The TAS includes an airport data base as well as a terrain data base that is structured to provide various resolutions depending on the topography of the particular geographic area of interest. Navigational data from a satellite-based navigational system, such as a global positioning system (GPS), is used to provide a LOOK-AHEAD/LOOK-DOWN and LOOK-UP terrain advisory and terrain warning indications based upon the current position and projected flight path of the aircraft. Since the terrain advisory and the warning signals are a function of the flight path of the aircraft, nuisance warnings are minimized.
更多17. GROUND PROXIMITY WARNING SYSTEM
申请号: PCT/US2001/023674
申请日: 2001-07-27
公开（公告）号: WO2002059546A1
公开（公告）日: 2002-08-01
发明人: CONNER, Kevin; ISHIHARA, Yasuo; JOHNSON, Steven, C.
A terrain avoidance system, method and computer program product for reducing nuisance alarms. The system includes a geometric altitude component, first and second vertical safety margin generators, and an alert component.
更多18. GROUND PROXIMITY WARNING SYSTEM
申请号: PCT/US2000/002566
申请日: 2000-02-01
公开（公告）号: WO00045126A1
公开（公告）日: 2000-08-03
发明人:
The present invention provides several apparatus, methods, and computer program products for determining a look ahead distance value for use in a ground proximity warning system. The apparatus, methods, and computer program products generate a candidate look ahead distance value that provides a constant reaction time for varying aircraft speeds. A processor generates the constant reaction time look ahead distance by multiplying a desired reaction time by the speed of the aircraft. This distance is compared by the processor to other candidate look ahead distance values that have variable reaction times for varying aircraft speeds. If the aircraft is traveling at a relatively high speed, the processor selects the constant reaction time look ahead distance value for use in the ground proximity warning system. The present invention can provide a look ahead distance value that reduces nuisance alarms for lower speeds, while also providing at least a minimum reaction time for higher speeds.
更多