作者: Richard D. Vandervoort , David S. Steiner
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摘要: Systems and methods for braking aircraft are disclosed. These systems can be employed on multi-main gear to reduce the radius with which makes low speed, pivot turns. Further used correct behavior of during a turn when actual or measured deviates from commanded turning behavior. For example, one system includes controller operatively coupleable amongst leftmost landing gear, rightmost an intermediate aircraft. The configured direct application brakes wheels left turn, release all turn. Another right brakes, is receive first signal corresponding behavior, second and, in response error value (based signals) exceeding threshold value, change force applied at least brakes.