Invention Grant
US08442701B2 Dynamic roll angle stall protection for an aircraft 有权
飞机的动态侧倾角失速保护

Dynamic roll angle stall protection for an aircraft
Abstract:
A method, apparatus, and computer program product are present for operating an aircraft. A roll angle limit is identified using a load factor selected to allow a lateral maneuvering capability of the aircraft by forming an identified roll angle limit in response to vertical maneuvering of the aircraft. The vertical maneuvering of the aircraft is performed using the identified roll angle limit.
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