Aeronautics and astronautics – Aircraft control – Automatic
Patent
1990-08-17
1992-03-17
Basinger, Sherman
Aeronautics and astronautics
Aircraft control
Automatic
244 76B, 364434, G05D 110
Patent
active
050961462
ABSTRACT:
A controller for generating a bank angle limit for an aircraft during takeoff with an nonoperational engine. The controller operates so that there are minimum and maximum bank angle limits. Between these minimum and maximums, there is a linear relationship between aircraft airspeed and bank angle limit. However, before there is a change in aircraft airspeed from an increasing mode to a decreasing mode or vice versa, the bank angle limit remains constant until the change in aircraft airspeed is greater than or equal to a predetermined airspeed differential.
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Nguyen Dung D.
Orgun Munir
Basinger Sherman
Donahue B. A.
Ellis Christopher P.
Sproule R. H.
The Boeing Company
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