-
1.发明授权公开(公告)号：US10482772B2
公开(公告)日：2019-11-19
申请号：US15786725
申请日：2017-10-18
发明人： Sanju Kumari , Minni Ambooken , Subhadeep Pal , Nithin Ambika
摘要： Methods and systems are provided for generating a flight profile for search and rescue (SAR) operations. The method comprises monitoring flight parameters of an in-flight aircraft engaged in star operations through the aircraft's flight management system (FMS). The flight parameters are transmitted to a ground-based FMS that accesses a terrain database and a real-time weather database. With this information, the ground-based FMS generates a star flight profile for the aircraft. The flight profile is then transmitted to the in-flight aircraft's FMS.
-
公开(公告)号：US09916032B2
公开(公告)日：2018-03-13
申请号：US15157520
申请日：2016-05-18
发明人： Sabu Mathew , Sunil Sulania , Nithin Ambika , Ashwini Kshitij
IPC分类号： G06F3/041 , G06F3/0488 , B64D43/00 , G08G5/00
CPC分类号： G06F3/0416 , B64D43/00 , G06F1/1626 , G06F1/1692 , G06F3/0362 , G06F3/0412 , G06F3/04847 , G06F3/0488 , G06F3/04883 , G06F3/04886 , G06F2203/0339 , G06F2203/04104 , G08G5/0086
摘要： A touchscreen display includes a first planar surface that comprises a first value-indicating virtual button showing a first value displayed in a first area of the first planar surface, a touch sensor operably coupled with the first planar surface, wherein the touch sensor is configured to detect a touch within the first area of the first planar surface, a second planar surface that is non-coplanar with respect to the first planar surface, the first and second planar surfaces forming a first common edge, a first swipe sensor operably coupled with the second planar surface, wherein the first swipe sensor is configured to detect a swiping motion in a first direction or in a second direction along the second planar surface, the second direction being opposite the first direction. The touchscreen display can be implemented in a vehicle, such as an aircraft.
-
公开(公告)号：US20170336901A1
公开(公告)日：2017-11-23
申请号：US15157520
申请日：2016-05-18
发明人： Sabu Mathew , Sunil Sulania , Nithin Ambika , Ashwini Kshitij
IPC分类号： G06F3/041 , B64D43/00 , G06F3/0488 , G08G5/00
CPC分类号： G06F3/0416 , B64D43/00 , G06F1/1626 , G06F1/1692 , G06F3/0362 , G06F3/0412 , G06F3/04847 , G06F3/0488 , G06F3/04883 , G06F3/04886 , G06F2203/0339 , G06F2203/04104 , G08G5/0086
摘要： A touchscreen display includes a first planar surface that comprises a first value-indicating virtual button showing a first value displayed in a first area of the first planar surface, a touch sensor operably coupled with the first planar surface, wherein the touch sensor is configured to detect a touch within the first area of the first planar surface, a second planar surface that is non-coplanar with respect to the first planar surface, the first and second planar surfaces forming a first common edge, a first swipe sensor operably coupled with the second planar surface, wherein the first swipe sensor is configured to detect a swiping motion in a first direction or in a second direction along the second planar surface, the second direction being opposite the first direction. The touchscreen display can be implemented in a vehicle, such as an aircraft.
-
公开(公告)号：US20190318638A1
公开(公告)日：2019-10-17
申请号：US16424089
申请日：2019-05-28
摘要： A system for providing obstacle alerts to an in-flight aircraft has been developed. The system includes a transceiver on board the vehicle that transmits performance parameters of the vehicle and a remotely located antenna that receives the performance parameters from the transceiver. Also included is a remotely located terrain database stores obstacle characteristics of terrestrial obstacles located in proximity to the vehicle. A remotely located computer system receives the performance parameters from the antenna and the obstacle characteristics in proximity to the vehicle from the terrain database. The computer system calculates a vehicle safety envelope based on the performance parameters and an obstacle safety envelope based on the obstacle characteristics. The computer system generates an obstacle alert for the vehicle if the vehicle safety envelope conflicts with the obstacle safety envelope.
-
5.发明授权公开(公告)号：US10347141B2
公开(公告)日：2019-07-09
申请号：US15498032
申请日：2017-04-26
摘要： A method for providing obstacle alerts to an in-flight aircraft has been developed. First, parameters of an in-flight aircraft are transmitted to a ground based processor station. The station calculates an aircraft safety envelope based on these parameters. The station accesses the characteristics of obstacles stored in a terrain database and calculates an obstacle safety envelope. Finally, the station determines if the aircraft safety envelope conflicts with the obstacle safety envelope and generates an alert for the aircraft if a conflict exists.
-
6.发明申请公开(公告)号：US20190114926A1
公开(公告)日：2019-04-18
申请号：US15786725
申请日：2017-10-18
发明人： Sanju Kumari , Minni Ambooken , Subhadeep Pal , Nithin Ambika
CPC分类号： G08G5/0013 , B64D43/00 , G01C23/005 , G08G5/0021 , G08G5/0026 , G08G5/0039 , G08G5/0043 , G08G5/0086 , G08G5/0091
摘要： Methods and systems are provided for generating a flight profile for search and rescue (SAR) operations. The method comprises monitoring flight parameters of an in-flight aircraft engaged in star operations through the aircraft's flight management system (FMS). The flight parameters are transmitted to a ground-based FMS that accesses a terrain database and a real-time weather database. With this information, the ground-based FMS generates a star flight profile for the aircraft. The flight profile is then transmitted to the in-flight aircraft's FMS.
-
7.发明申请公开(公告)号：US20180315324A1
公开(公告)日：2018-11-01
申请号：US15498032
申请日：2017-04-26
CPC分类号： G08G5/04 , B64C39/024 , B64C2201/141 , B64C2201/146 , G05D1/0011 , G05D1/0088 , G05D1/0202 , G08G1/165 , G08G5/0013 , G08G5/0086 , G08G9/02
摘要： A method for providing obstacle alerts to an in-flight aircraft has been developed. First, parameters of an in-flight aircraft are transmitted to a ground based processor station. The station calculates an aircraft safety envelope based on these parameters. The station accesses the characteristics of obstacles stored in a terrain database and calculates an obstacle safety envelope. Finally, the station determines if the aircraft safety envelope conflicts with the obstacle safety envelope and generates an alert for the aircraft if a conflict exists.
-
-
-
-
-
-
搜索结果
7 条记录 (耗时 0.016 秒)
