Aircraft state monitoring method, device, equipment and medium

The invention discloses an aircraft state monitoring method, device and equipment and a medium. When an aircraft is on the ground, an aviation auxiliary power system and a vibration source sensor are started; resonance data of the aircraft are obtained through detection of a vibration source sensor,...

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Bibliographische Detailangaben
Hauptverfasser: GONG XIAOFENG, YUAN YINPU, TAN YINGHUA, GUO MING, MEI JIE, ZHONG YONGJIANG, LYU HONGRU, QIAO JIAMIN, YUAN ZHONGDA, LI MUFEI, LIU AOTIAN
Format: Patent
Sprache:chi ; eng
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Beschreibung
Zusammenfassung:The invention discloses an aircraft state monitoring method, device and equipment and a medium. When an aircraft is on the ground, an aviation auxiliary power system and a vibration source sensor are started; resonance data of the aircraft are obtained through detection of a vibration source sensor, and working data of an aviation auxiliary power system, all systems of the aircraft and a control surface are obtained; determining a working state, a structural state and a mechanical state of the aircraft according to the resonance data and the working data; starting a cockpit terminal display, and performing butt-joint debugging on the cockpit terminal display and the control tower terminal display; and the working state, the structural state and the mechanical state of the aircraft are displayed through the cockpit terminal display and the control tower terminal display. According to the method, various state data of the aircraft can be effectively recorded, the state result of the aircraft can be intuitively