Disclosed is a method for controlling minimum-radius limitation turning of an airplane through differential braking. According to a friction coefficient of a tire and a track, visualized braking pressure and turning linear speed control parameters are provided for an aviator, and rapid turning of the airplane with the structurally-allowable minimum turning radius is achieved. Maneuverability and safety of the airplane turning process controlled by the aviator on the ground through the differential braking are ensured.
Method for controlling minimum-radius limitation turning of airplane through differential braking
2015-11-25
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
Airplane turning limitation control method through differential braking
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