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1. 发明公开

EP2778607A3 Method of calibrating a heading reference system 审中-公开
标题翻译：校准航向参考系统的方法
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
申请人： Innovative Solutions and Support, Inc.
发明人： Askarpour, Shahram
IPC分类号： G01C17/38 , G01C21/20
CPC分类号： G01C25/00 , G01C17/38 , G01C21/20
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。

2. 发明公开

EP2778607A2 Method of calibrating a heading reference system 审中-公开
标题翻译： 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
申请人： Innovative Solutions and Support, Inc.
发明人： Askarpour, Shahram
IPC分类号： G01C17/38
CPC分类号： G01C25/00 , G01C17/38 , G01C21/20
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。

3. 发明授权

EP2525337B1 Upgraded flight management system and method of providing the same 有权
公开(公告)号：EP2525337B1
公开(公告)日：2019-10-09
申请号：EP12161737.7
申请日：2012-03-28
申请人： Innovative Solutions and Support, Inc.
发明人： Hedrick, Geoffrey S.M. , Askarpour, Shahram , Knopf, Markus
IPC分类号： G08G5/00

4. 发明授权

EP2778070B1 Composite normalized angle of attack indicating system 有权
公开(公告)号：EP2778070B1
公开(公告)日：2017-08-16
申请号：EP13193791.4
申请日：2013-11-21
申请人： Innovative Solutions and Support, Inc.
发明人： Hedrick, Geoffrey S.M. , Askarpour, Shahram
IPC分类号： B64D43/02 , G01P13/02
CPC分类号： B64D43/02 , B64D45/00 , F01D21/003 , G01D13/12 , G01D13/22 , G01P13/025
摘要： A composite normalized angle of attack indicating system provides a simultaneous display of both body angle of attack, such as in digital form, and normalized angle of attack for an aircraft. The display may be visually enhanced as stall is approached such as by zooming the body angle of attack digital display and/or by changing the color of the display. The normalized display also selectively displays an approach reference band when the flap setting is equal to or greater than 20 degrees.

5. 发明公开

EP2525337A2 Upgraded flight management system and method of providing the same 有权
标题翻译： AufgerüstetesFlugmanagementsystem und Verfahren zur Bereitstellung davon
公开(公告)号：EP2525337A2
公开(公告)日：2012-11-21
申请号：EP12161737.7
申请日：2012-03-28
申请人： Innovative Solutions and Support, Inc.
发明人： Hedrick, Geoffrey S.M. , Askarpour, Shahram , Knopf, Markus
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.
摘要翻译：可以升级预先存在的FMS系统以增加其功能，同时仍然利用先前在飞机上提供的遗留系统的某些组件，并用不同的组件替换其他预先存在的组件，以增强FMS系统的功能。升级的FMS系统中的现有IRU，CADC，DME接收器和DFGC与传统AFMC通信，而不是采用现有的FMS系统中存在的传统EFIS，EFIS被数据集中器单元以及显示控制面板和集成平板显示器，以及GPS接收器。升级的FMS系统能够增加功能，例如使用基于GPS的导航解决方案和RTA功能增加导航数据库存储容量，RNP，VNAV和RNAV功能，同时仍能使传统AFMC在整个飞行中利用其飞机性能。

6. 发明公开

EP2284494A3 Aircraft panel display system with graphical image integrity 有权转让
标题翻译：与图形图像完整性的飞行器控制面板显示系统
公开(公告)号：EP2284494A3
公开(公告)日：2012-07-18
申请号：EP10014609.1
申请日：2006-06-27
申请人： Innovative Solutions and Support, Inc.
发明人： Hedrick, Geoffrey S.M. , Askarpour, Shahram , Knopf, Markus , Collins, Jeff
IPC分类号： G01C23/00 , G06F3/14 , G09G5/00
CPC分类号： G06F3/1415 , G01C23/00 , G09G2330/12 , G09G2340/10 , G09G2360/18 , G09G2380/12
摘要： An improvement over prior art aircraft instrument flight display systems for imaging on a bitmapped display formed of a multiplicity of individually addressable pixels at locations throughout the display and actuatable to create images on the display, employs a common processor operatively connected between a video graphics processor and the display system input of a common set of aircraft and environmental sensor data - to provide both an integrity checking function and a graphics rendering function in which the integrity checking function can directly check the images generated by the graphics rendering function without the need for comparator hardware. Separate processors may also be employed instead of a common processor. The integrity checking function uses the input information for generating a pixel verification map for checking the display based on pixel color and location. The system can also check for pitch and roll accuracy as well as check the integrity of complex images using statistical detection.

7. 发明公开

EP2778070A1 Composite normalized angle of attack indicating system 有权
标题翻译：综合归一化攻角指示系统
公开(公告)号：EP2778070A1
公开(公告)日：2014-09-17
申请号：EP13193791.4
申请日：2013-11-21
申请人： Innovative Solutions and Support, Inc.
发明人： Hedrick, Geoffrey S.M. , Askarpour, Shahram
IPC分类号： B64D43/02 , G01P13/02
CPC分类号： B64D43/02 , B64D45/00 , F01D21/003 , G01D13/12 , G01D13/22 , G01P13/025
摘要： A composite normalized angle of attack indicating system provides a simultaneous display of both body angle of attack, such as in digital form, and normalized angle of attack for an aircraft. The display may be visually enhanced as stall is approached such as by zooming the body angle of attack digital display and/or by changing the color of the display. The normalized display also selectively displays an approach reference band when the flap setting is equal to or greater than 20 degrees.
摘要翻译：综合标准化迎角指示系统提供了同时显示诸如数字形式的两种身体迎角，以及飞机的正常化迎角。当靠近失速时，例如通过缩小身体迎角数字显示和/或通过改变显示的颜色，可以在视觉上增强显示。当襟翼设置等于或大于20度时，标准化显示还选择性地显示接近参考频带。

8. 发明公开

EP1757906A3 Aircraft panel display system with graphical image integrity 有权
标题翻译：与图形图像完整性的飞行器控制面板显示系统
公开(公告)号：EP1757906A3
公开(公告)日：2010-06-30
申请号：EP06253352.6
申请日：2006-06-27
申请人： Innovative Solutions and Support, Inc.
发明人： Hedrick, Geoffrey S M , Askarpour, Shahram , Knopf, Markus , Collins, Jeff
IPC分类号： G01C23/00
CPC分类号： G06F3/1415 , G01C23/00 , G09G2330/12 , G09G2340/10 , G09G2360/18 , G09G2380/12
摘要： An improvement over prior art aircraft instrument flight display systems for imaging on a bitmapped display formed of a multiplicity of individually addressable pixels at locations throughout the display and actuatable to create images on the display, employs a common processor operatively connected between a video graphics processor and the display system input of a common set of aircraft and environmental sensor data - to provide both an integrity checking function and a graphics rendering function in which the integrity checking function can directly check the images generated by the graphics rendering function without the need for comparator hardware. Separate processors may also be employed instead of a common processor. The integrity checking function uses the input information for generating a pixel verification map for checking the display based on pixel color and location. The system can also check for pitch and roll accuracy as well as check the integrity of complex images using statistical detection.

9. 发明公开

EP2525337A3 Upgraded flight management system and method of providing the same 有权
标题翻译：升级飞行管理系统及其方法，用于提供
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
申请人： Innovative Solutions and Support, Inc.
发明人： Hedrick, Geoffrey S.M. , Askarpour, Shahram , Knopf, Markus
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.

10. 发明授权

EP1757906B1 Aircraft panel display system with graphical image integrity 有权
标题翻译：与图形图像完整性的飞行器控制面板显示系统
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
申请人： Innovative Solutions and Support, Inc.
发明人： Hedrick, Geoffrey S M , Askarpour, Shahram , Knopf, Markus , Collins, Jeff
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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