General aircraft attitude teaching platform and system

The invention discloses a general aircraft attitude teaching platform and system. The teaching platform comprises a bearing platform, a receiving platform, a fixing base, a two-degree-of-freedom parallel mechanism, a central supporting rod, a direction rotating plate, a spherical hinge, a Hooke hing...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: CHEN JUNRUI, SUN CHENWU, LI CHENRONG, WU YICHAO, DAI XING'AN
Format: Patent
Sprache:chi ; eng
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Beschreibung
Zusammenfassung:The invention discloses a general aircraft attitude teaching platform and system. The teaching platform comprises a bearing platform, a receiving platform, a fixing base, a two-degree-of-freedom parallel mechanism, a central supporting rod, a direction rotating plate, a spherical hinge, a Hooke hinge, a DD motor and an electric conducting sliding ring, and the bearing platform, the receiving platform and the fixing base are arranged from top to bottom in sequence. The two-degree-of-freedom parallel mechanism is composed of two high-precision servo electric cylinders; the central supporting rodis arranged between the receiving platform and the bearing platform, the two ends of the parallel mechanism are fixedly connected with the receiving platform and the bearing platform through the Hooke hinge and the spherical hinge respectively, and the direction rotating plate is driven by the angular-second high-precision DD motor to independently complete the heading degree of freedom. The system is simple and reliable