Locking a bank angle parameter and a ground speed parameter
AssigneeThe Boeing Company
InventorsSalvador RAMIREZ BLANCO, Daniel MIGUEL, Sergio VILLANUEVA, Binh Quang An BUI
Life of this patent
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AssigneeThe Boeing Company
InventorsSalvador RAMIREZ BLANCO, Daniel MIGUEL, Sergio VILLANUEVA, Binh Quang An BUI
Estimating the term…
A flight management system (FMS) of an aircraft may determine that a leg of a lateral trajectory profile, of a flight plan for the aircraft, is active. The FMS may determine, based on determining that the leg of the lateral trajectory profile is active, that a lateral distance between the aircraft and an end waypoint associated with the leg satisfies a lateral distance threshold and may therefore perform an update to the lateral trajectory profile to lock a bank angle parameter to a particular bank angle value. The FMS may determine that a transition, which is associated with the end waypoint and another leg of the lateral trajectory profile, is active and may therefore perform an update to the lateral trajectory profile to lock a ground speed parameter to a particular ground speed value.
A flight management system (FMS) of an aircraft, comprising:
A non-transitory computer-readable medium storing a set of instructions, the set of instructions comprising:
A method, comprising:
Dependencies are inferred from the claim text.