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公开(公告)号：US11142337B2
公开(公告)日：2021-10-12
申请号：US16037214
申请日：2018-07-17
摘要： A method and system of determining or estimating a descent profile includes receiving a final approach fix for a target destination, repeatedly back-calculating a set of subsequent models, determining a descent profile based on the repeated back-calculating the set of subsequent models, and operating the aircraft in accordance with the descent profile.
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公开(公告)号：US20200023994A1
公开(公告)日：2020-01-23
申请号：US16037214
申请日：2018-07-17
摘要： A method and system of determining or estimating a descent profile includes receiving a final approach fix for a target destination, repeatedly back-calculating a set of subsequent models, determining a descent profile based on the repeated back-calculating the set of subsequent models, and operating the aircraft in accordance with the descent profile.
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公开(公告)号：US20200026307A1
公开(公告)日：2020-01-23
申请号：US16037234
申请日：2018-07-17
发明人： David Michael Lax , Reza Ghaemi , Pierino Gianni Bonanni , Nicholas Race Visser , Owen Michael O'Keefe
摘要： A method and system of determining or predicting a climb profile for an aircraft, includes receiving, by a controller module, an initial climb profile defining a portion of a flight plan for the aircraft between takeoff and a cruise profile, and an altitude climb constraint defining at least one altitude limitation of the aircraft, determining, by the controller module, that the initial climb profile does not satisfy the altitude constraint, and determining an updated climb profile based on a set of subsequent climb models.
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公开(公告)号：US10935984B2
公开(公告)日：2021-03-02
申请号：US16037234
申请日：2018-07-17
发明人： David Michael Lax , Reza Ghaemi , Pierino Gianni Bonanni , Nicholas Race Visser , Owen Michael O'Keefe
摘要： A method and system of determining or predicting a climb profile for an aircraft, includes receiving, by a controller module, an initial climb profile defining a portion of a flight plan for the aircraft between takeoff and a cruise profile, and an altitude climb constraint defining at least one altitude limitation of the aircraft, determining, by the controller module, that the initial climb profile does not satisfy the altitude constraint, and determining an updated climb profile based on a set of subsequent climb models.
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