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公开(公告)号：US11745896B2
公开(公告)日：2023-09-05
申请号：US17930124
申请日：2022-09-07
发明人： Michael Mast , Yuta Morioka , Martin Jezek , Jeffrey Glenn
CPC分类号： B64D45/00 , B64D43/02 , B64D45/08 , G05D1/105 , G08G5/0047 , G08G5/025 , B64D2045/0085
摘要： Flight guidance systems and methods that provide an airport selection in response to an EO condition in a single engine plane. The airport selection takes into consideration factors such as optimal approach type, runway length, weather, terrain, remaining battery time, and the like. Additionally, various also generate and display a visual indication of a remaining glide range when the EO condition is happening; the remaining glide range determination is based, at least in part, on terrain.
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公开(公告)号：US11511883B2
公开(公告)日：2022-11-29
申请号：US17179957
申请日：2021-02-19
发明人： Michael Mast , Yuta Morioka , Martin Jezek , Jeffrey Glenn
摘要： Flight guidance systems and methods that provide an airport selection in response to an EO condition in a single engine plane. The airport selection takes into consideration factors such as optimal approach type, runway length, weather, terrain, remaining battery time, and the like. Additionally, various also generate and display a visual indication of a remaining glide range when the EO condition is happening; the remaining glide range determination is based, at least in part, on terrain.
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公开(公告)号：US20240274018A1
公开(公告)日：2024-08-15
申请号：US18646203
申请日：2024-04-25
发明人： Michael Mast , Yuta Morioka , Jeffrey Glenn
摘要： Flight guidance methods, systems, and aircraft systems providing assist-to-land and emergency land (EL) functions. The method includes generating a visual indication of the availability and status of an assist-to-land function and an EL function when the current altitude of the aircraft exceeds an altitude threshold. When in assist-to-land, visual and audible flight guidance can be generated to guide the pilot to a safe landing at a selected runway or at a best runway for the conditions. Functions can be activated by user manipulations of interface objects and/or by software determinations. Software determinations to enter the EL function can automatically control the flying of the aircraft along an approach profile to a safe landing at a nearest suitable airport. EL determinations can be made based on pilot incapacitation.
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公开(公告)号：US20210287560A1
公开(公告)日：2021-09-16
申请号：US17180954
申请日：2021-02-22
发明人： Michael Mast , Yuta Morioka , Jeffrey Glenn
摘要： Flight guidance methods, systems, and aircraft systems providing assist-to-land and emergency land (EL) functions. The method includes generating a visual indication of the availability and status of an assist-to-land function and an EL function when the current altitude of the aircraft exceeds an altitude threshold. When in assist-to-land, visual and audible flight guidance can be generated to guide the pilot to a safe landing at a selected runway or at a best runway for the conditions. Functions can be activated by user manipulations of interface objects and/or by software determinations. Software determinations to enter the EL function can automatically control the flying of the aircraft along an approach profile to a safe landing at a nearest suitable airport. EL determinations can be made based on pilot incapacitation.
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公开(公告)号：US12020583B2
公开(公告)日：2024-06-25
申请号：US17180954
申请日：2021-02-22
发明人： Michael Mast , Yuta Morioka , Jeffrey Glenn
CPC分类号： G08G5/025 , B64C9/00 , B64C13/16 , B64D43/00 , B64D45/08 , G05D1/042 , G05D1/101 , G08G5/0013
摘要： Flight guidance methods, systems, and aircraft systems providing assist-to-land and emergency land (EL) functions. The method includes generating a visual indication of the availability and status of an assist-to-land function and an EL function when the current altitude of the aircraft exceeds an altitude threshold. When in assist-to-land, visual and audible flight guidance can be generated to guide the pilot to a safe landing at a selected runway or at a best runway for the conditions. Functions can be activated by user manipulations of interface objects and/or by software determinations. Software determinations to enter the EL function can automatically control the flying of the aircraft along an approach profile to a safe landing at a nearest suitable airport. EL determinations can be made based on pilot incapacitation.
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公开(公告)号：US20230002071A1
公开(公告)日：2023-01-05
申请号：US17930124
申请日：2022-09-07
发明人： Michael Mast , Yuta Morioka , Martin Jezek , Jeffrey Glenn
摘要： Flight guidance systems and methods that provide an airport selection in response to an EO condition in a single engine plane. The airport selection takes into consideration factors such as optimal approach type, runway length, weather, terrain, remaining battery time, and the like. Additionally, various also generate and display a visual indication of a remaining glide range when the EO condition is happening; the remaining glide range determination is based, at least in part, on terrain.
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公开(公告)号：US20210276728A1
公开(公告)日：2021-09-09
申请号：US17179957
申请日：2021-02-19
发明人： Michael Mast , Yuta Morioka , Martin Jezek , Jeffrey Glenn
摘要： Flight guidance systems and methods that provide an airport selection in response to an EO condition in a single engine plane. The airport selection takes into consideration factors such as optimal approach type, runway length, weather, terrain, remaining battery time, and the like. Additionally, various also generate and display a visual indication of a remaining glide range when the EO condition is happening; the remaining glide range determination is based, at least in part, on terrain.
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