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公开(公告)号：EP1908021B1
公开(公告)日：2018-07-11
申请号：EP06787759.7
申请日：2006-07-18
CPC分类号： G01C23/005 , G06F3/14 , G06F3/1415 , G09G5/363 , G09G2320/02 , G09G2330/12 , G09G2380/12
摘要： An aircraft cockpit flight deck data display system for displaying, on a viewable display screen, typically anti-aliased graphical imaging data derived from aircraft sensors, generates or receives graphics processing language (GPL) commands that define the information intended for presentation on the display screen. The GPL commands are input to a video graphics processor that is operable to interpret the received GPL commands and to generate therefrom video imaging data transferable to the display screen to populate the screen with the intended information. The same GPL commands are also input to a comparator processor that is operable to interpret the received GPL commands and to generate therefrom selected "points of light", comprising a limited subset of the video imaging data generated by the video graphics processor. The comparator processor-generated "points of light" are then compared to the respective corresponding video imaging data points generated by the video graphics processor to thereby validate the proper operation of the video graphics processor and the accuracy of the video imaging data generated by the video graphics processor.
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公开(公告)号：EP2778607A3
公开(公告)日：2014-11-19
申请号：EP14150336.7
申请日：2014-01-07
发明人： Askarpour, Shahram
摘要： A method of calibrating a vehicle's heading system, such as the attitude heading and reference system of an aircraft or the heading system of a ship, positioned along the Earth's surface involves obtaining both actual and theoretical readings for the magnetometer of the heading system, and comparing these values to obtain calibration values for the heading system which are then averaged to obtain a universal average gain and offset for the magnetometer. The vehicle may be repositioned, such as to North, South, East, and west magnetic headings, with the procedure repeated at each of these headings, and the calibration values averaged, further increasing the accuracy.
摘要翻译： 校准诸如沿着地球表面定位的飞机的姿态航向和参考系统或船的航向系统的车辆航向系统的方法涉及获得航向系统的磁力计的实际和理论读数以及比较 这些值用于获得航向系统的校准值，然后将其平均以获得磁力计的通用平均增益和偏移。 车辆可以重新定位，例如北向，南向，东向和西向的磁航向，并在这些航向的每一个处重复该过程，并将校准值取平均值，进一步提高精度。
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3.发明公开Method of calibrating a heading reference system 审中-公开Verfahren zur Kalibrierung eines Kursreferenzsystems
公开(公告)号：EP2778607A2
公开(公告)日：2014-09-17
申请号：EP14150336.7
申请日：2014-01-07
发明人： Askarpour, Shahram
IPC分类号： G01C17/38
摘要： A method of calibrating a vehicle's heading system, such as the attitude heading and reference system of an aircraft or the heading system of a ship, positioned along the Earth's surface involves obtaining both actual and theoretical readings for the magnetometer of the heading system, and comparing these values to obtain calibration values for the heading system which are then averaged to obtain a universal average gain and offset for the magnetometer. The vehicle may be repositioned, such as to North, South, East, and west magnetic headings, with the procedure repeated at each of these headings, and the calibration values averaged, further increasing the accuracy.
摘要翻译： 一种校准车辆航向系统的方法，例如飞机的姿态航向和参考系统或沿着地球表面的船舶航向系统，包括获得航向系统的磁力计的实际和理论读数，并比较 这些值用于获得标题系统的校准值，然后对其进行平均，以获得磁力计的通用平均增益和偏移。 可以重新定位车辆，例如北，南，东，西磁标题，其中每个标题都重复进行，平均校准值进一步提高。
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4.发明授权
公开(公告)号：EP1373850B1
公开(公告)日：2012-01-25
申请号：EP02746300.9
申请日：2002-03-01
IPC分类号： G01C5/06
CPC分类号： G01C25/005 , G01C5/005
摘要： In an aircraft conventionally-including a redundant pair of independent primary altitude determination systems of accuracy certified for RVSM operations, an initially loosely calibrated backup altimeter (32) receives independent static pressure data for use in calculating altitude.
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公开(公告)号：EP1490860B1
公开(公告)日：2010-12-15
申请号：EP03713699.1
申请日：2003-02-27
IPC分类号： G02F1/1335
CPC分类号： G02F1/133502 , G02F1/133504 , G02F2201/38 , G02F2202/28
摘要： An improved flat panel display provides reduced reflection of incident light on the display to improve visibility. The display includes a transparent top cover panel such as glass which is bonded or laminated to the display polarizer. The outer viewing surface of the top cover panel carries a plurality of integral surface features defined in the surface, which may comprise etched bumps or micro-machined tetrahedron-shaped protuberances that may be truncated, smoothed, and/or variously oriented and sized to further reduce incident light reflectivity. A multi-layer HEA coating on the featured surface defines a graduated transition layer with an index of refraction that gradually, and preferably smoothly, varies from layer to layer of the HEA coating from the index of refraction of the top cover panel to the index of refraction of the ambient air or other material which the outermost viewable surface of the display presents an image to an observer or viewer.
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公开(公告)号：EP2525337A3
公开(公告)日：2016-04-06
申请号：EP12161737.7
申请日：2012-03-28
IPC分类号： G08G5/00
CPC分类号： G08G5/003 , G01S19/13 , G05D1/0077 , G06F16/951 , G08G5/0021 , G08G5/0034 , G08G5/0047
摘要： A preexisting FMS system may be upgraded to increase its functionality while still taking advantage of certain components of the legacy system previously provided on the aircraft and replacing other preexisting components with different components for enhancing the functionality of the FMS system. The preexisting IRU, CADC, DME receiver and DFGC in the upgraded FMS system are in communication with the legacy AFMC but, instead of employing the legacy EFIS which existed in the prrexisting FMS system, the EFIS is replaced by a data concentrator unit as well as the display control panel and integrated flat panel display, and a GPS receiver. The upgraded FMS system is capable of such increased functionality as increased navigation database storage capacity, RNP, VNAV and RNAV capability utilizing a GPS based navigation solution, and RTA capability, while still enabling the legacy AFMC to exploit its aircraft performance capabilities throughout the flight.
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8.发明公开
公开(公告)号：EP2402716A3
公开(公告)日：2013-12-18
申请号：EP11160361.9
申请日：2011-03-30
CPC分类号： B64D45/00 , B60K37/02 , B60K2350/1072 , B64D43/00 , G01C23/00 , G01D7/002 , G06F3/04847 , G06F2203/04805 , G09G3/20 , G09G2340/0407 , G09G2340/045
摘要： A method and system for highlighting a parameter image representative of a flight parameter of an aircraft to a user in a multi-parameter aircraft instrument display, such as a flat panel display. An electronic instrument display is configured to present parameter images, at least one of which includes a first indicator configured to indicate a specific value (e.g., a target value) for a flight parameter and a second indicator configured to indicate an actual flight parameter value that changes according to variations in the flight parameter. A graphics rendering controller is configured to generate the parameter images and to enlarge a portion of the parameter image when the actual flight parameter value is within a predetermined range from the target value.
摘要翻译： 诸如平板显示器：一种用于在多参数飞机仪表显示高亮参数图像代表的飞机的飞行参数的给用户，颜色的方法和系统。 的电子设备显示被配置成呈现参数的图像，其中至少一个包括配置成指示特定值的第一指示符（例如，目标值）为飞行参数和第二指示符配置为指示实际飞行参数值做 变化gemäß在飞行参数的变化。 图形渲染控制器被配置为产生所述参数和图像当实际飞行参数值是从所述目标值的预定范围内放大参数图像的一部分。
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公开(公告)号：EP1373832B1
公开(公告)日：2012-01-25
申请号：EP02725060.4
申请日：2002-03-01
IPC分类号： G01C5/06
CPC分类号： G01C5/005
摘要： The altimeters (28, 30) which contain within it means for storing the Static Source Error Correction (SSEC) includes means for downloading the SSEC and for transferring it to a new altimeter (32) which may then be used in the place of one of the original altimeters (28, 30) without losing the information built up over time or having to re-calibrate the new altimeter (32) based on new tests. The altimeters (28, 30) also include means for uploading a known SSEC thereto.
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公开(公告)号：EP1757906B1
公开(公告)日：2011-12-21
申请号：EP06253352.6
申请日：2006-06-27
IPC分类号： G01C23/00
CPC分类号： G06F3/1415 , G01C23/00 , G09G2330/12 , G09G2340/10 , G09G2360/18 , G09G2380/12
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