Multi-structure aircraft self-adaptive anti-skid brake control method, system, equipment, program product and medium
The invention relates to the technical field of airplane wheel braking, in particular to a multi-structure airplane self-adaption anti-skid braking control method, system, device, program product and medium, and the method comprises the steps that the expected speed reduction rate of an airplane, th...
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Format: | Patent |
Sprache: | chi ; eng |
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Zusammenfassung: | The invention relates to the technical field of airplane wheel braking, in particular to a multi-structure airplane self-adaption anti-skid braking control method, system, device, program product and medium, and the method comprises the steps that the expected speed reduction rate of an airplane, the real-time speed reduction rate of airplane wheels and the real-time speed reduction rate of the airplane are obtained; determining whether the airplane wheel is in a slipping state; when the airplane wheels are in the slipping state, anti-lock control is conducted on the airplane wheels; when the airplane wheels are not in the slipping state, PI control over the airplane deceleration rate is carried out, and pressurization is carried out according to the preset pressurization speed or the current brake pressure is kept. According to the invention, the control mode is adaptively switched when the operation scene, the runway state and the operation working condition are different, so that the safe and stable brakin |
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