发明名称 |
DYNAMIC ROLL ANGLE STALL PROTECTION FOR AN AIRCRAFT |
摘要 |
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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申请公布号 |
US2010087970(A1) |
申请公布日期 |
2010.04.08 |
申请号 |
US20080244257 |
申请日期 |
2008.10.02 |
申请人 |
BLECHEN FREDERICK CHARLES HENRY |
发明人 |
BLECHEN FREDERICK CHARLES HENRY |
分类号 |
G05D1/08 |
主分类号 |
G05D1/08 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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