-
1.发明授权Methods and systems for distinguishing ARINC 743 from ARINC 743A protocols 有权ARINC 743与ARINC 743A协议区别的方法和系统公开(公告)号：US07355550B1
公开(公告)日：2008-04-08
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： G01S5/02
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。
-
2.发明授权Variable enhanced ground proximity warning system look-ahead offset and sub-offset 有权可变增强型接地预警系统先行偏移和子偏移公开(公告)号：US07205906B2
公开(公告)日：2007-04-17
申请号：US09916630
申请日：2001-07-27
申请人： Steve C. Johnson , Yasuo Ishihara , Kevin J Conner
发明人： Steve C. Johnson , Yasuo Ishihara , Kevin J Conner
IPC分类号： G08B23/00
CPC分类号： G05D1/0676 , G01C5/005
摘要： The present invention includes a system, method and computer program product for reducing nuisance warnings during low altitude flight conditions and in the presence of low position uncertainty. The system includes a first component that determines whether the aircraft is in a low altitude flight condition and a second component that determines the position, positional uncertainty, and the heading. The system also includes a third component that attenuates and refines the look-ahead envelope in accord with the determined condition of flight and positional uncertainty.
摘要翻译： 本发明包括用于在低空飞行条件下和存在低位置不确定性的情况下减少有害警告的系统，方法和计算机程序产品。 该系统包括确定飞机是否处于低空飞行状态的第一部件和确定位置，位置不确定性和航向的第二部件。 该系统还包括根据确定的飞行条件和位置不确定性来衰减和提炼先行信封的第三部件。
-
公开(公告)号：US08271191B2
公开(公告)日：2012-09-18
申请号：US11426547
申请日：2006-06-26
申请人： Yasuo Ishihara , Kevin J Conner , Steve C. Johnson
发明人： Yasuo Ishihara , Kevin J Conner , Steve C. Johnson
IPC分类号： G01C23/00
摘要： Methods and systems for determining reliability of Global Positioning System (GPS) ground speed. An example system receives GPS track information and GPS ground speed, determines a change in GPS track information and determines reliability of the GPS ground speed based on the determined change in GPS track information relative to the GPS ground speed. The system sets a GPS ground speed based on the determined reliability. A GPS ground speed output is set to zero, if the GPS ground speed is determined unreliable and the GPS ground speed output is set to the GPS ground speed, if the GPS ground speed is determined reliable. The system sends the GPS ground speed output to a Runway Awareness and Advisory System (RAAS). Also, the system sets the GPS ground speed output to zero, if a received GPS ground speed validity signal or a received GPS track validity signal indicate invalid.
摘要翻译： 确定全球定位系统（GPS）地面速度的可靠性的方法和系统。 示例系统接收GPS轨道信息和GPS地面速度，确定GPS轨道信息的变化，并且基于GPS轨迹信息相对于GPS地面速度确定的变化来确定GPS地面速度的可靠性。 系统根据确定的可靠性设置GPS地面速度。 如果GPS地面速度被确定为可靠，则GPS地面速度输出被设置为零，如果GPS地面速度被确定为不可靠，并且将GPS地面速度输出设置为GPS地面速度。 系统将GPS地面速度输出发送到跑道意识和咨询系统（RAAS）。 此外，如果接收的GPS地面速度有效信号或接收的GPS轨道有效信号指示无效，则系统将GPS地面速度输出设置为零。
-
公开(公告)号：US20080176501A1
公开(公告)日：2008-07-24
申请号：US11625764
申请日：2007-01-22
IPC分类号： B64D13/02
CPC分类号： B64D13/02
摘要： Systems and methods for intelligently alerting the flight crew of a cabin depressurization. An example system includes a cabin altimeter that generates a cabin pressure value, an alerting device, such as a speaker system and a processing device in data communication with the cabin altimeter and the alerting device. The processing device determines if there is a problem with the cabin pressure received from the cabin altimeter, determines rate of change of the cabin pressure, and sets at least one of an alert volume or an alert frequency based on the cabin pressure and the rate of change of the cabin pressure if it was determined that a problem exists with the cabin pressure. The processing device also issues a cabin depressurization alert over the alerting device based on at least one of the set alert volume or alert frequency, if there is a problem with the cabin pressure value.
摘要翻译： 机舱减压的飞行机组智能报警的系统和方法。 示例系统包括产生客舱压力值的舱高度计，诸如扬声器系统的报警设备和与客舱高度计和报警设备进行数据通信的处理设备。 处理装置确定从客舱高度计接收到的客舱压力是否存在问题，确定客舱压力的变化率，并且基于客舱压力和车厢压力的速率来设置报警量或报警频率中的至少一个 如果确定客舱压力存在问题，则更改客舱压力。 如果存在舱室压力值的问题，则处理装置还基于设定的报警量或警报频率中的至少一个，在警报装置上发出舱室减压警报。
-
公开(公告)号：US20070299608A1
公开(公告)日：2007-12-27
申请号：US11426547
申请日：2006-06-26
IPC分类号： G01C23/00
摘要： Methods and systems for determining reliability of Global Positioning System (GPS) ground speed. An example system receives GPS track information and GPS ground speed, determines a change in GPS track information and determines reliability of the GPS ground speed based on the determined change in GPS track information relative to the GPS ground speed. The system sets a GPS ground speed based on the determined reliability. A GPS ground speed output is set to zero, if the GPS ground speed is determined unreliable and the GPS ground speed output is set to the GPS ground speed, if the GPS ground speed is determined reliable. The system sends the GPS ground speed output to a Runway Awareness and Advisory System (RAAS). Also, the system sets the GPS ground speed output to zero, if a received GPS ground speed validity signal or a received GPS track validity signal indicate invalid.
摘要翻译： 确定全球定位系统（GPS）地面速度的可靠性的方法和系统。 示例系统接收GPS轨道信息和GPS地面速度，确定GPS轨道信息的变化，并且基于GPS轨迹信息相对于GPS地面速度确定的变化来确定GPS地面速度的可靠性。 系统根据确定的可靠性设置GPS地面速度。 如果GPS地面速度被确定为可靠，则GPS地面速度输出被设置为零，如果GPS地面速度被确定为不可靠，并且将GPS地面速度输出设置为GPS地面速度。 系统将GPS地面速度输出发送到跑道意识和咨询系统（RAAS）。 此外，如果接收的GPS地面速度有效信号或接收的GPS轨道有效信号指示无效，则系统将GPS地面速度输出设置为零。
-
公开(公告)号：US06577931B2
公开(公告)日：2003-06-10
申请号：US09917374
申请日：2001-07-27
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： G08G504
CPC分类号： G01C5/005 , G05D1/0607
摘要： 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.
-
7.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。
-
8.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。
-
9.发明授权公开(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
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。
-
公开(公告)号：US09809313B2
公开(公告)日：2017-11-07
申请号：US11625764
申请日：2007-01-22
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： B64D13/02
CPC分类号： B64D13/02
摘要： Systems and methods for intelligently alerting the flight crew of a cabin depressurization. An example system includes a cabin altimeter that generates a cabin pressure value, an alerting device, such as a speaker system and a processing device in data communication with the cabin altimeter and the alerting device. The processing device determines if there is a problem with the cabin pressure received from the cabin altimeter, determines rate of change of the cabin pressure, and sets at least one of an alert volume or an alert frequency based on the cabin pressure and the rate of change of the cabin pressure if it was determined that a problem exists with the cabin pressure. The processing device also issues a cabin depressurization alert over the alerting device based on at least one of the set alert volume or alert frequency, if there is a problem with the cabin pressure value.
-
-
-
-
-
-
-
-
-
搜索结果
24 条记录 (耗时 0.017 秒)