The invention relates to a guidance-model-based fixed-wing unmanned aerial vehicle monitoring system comprising a hardware part and a software part. The hardware part and the software part are compatible to each other. The hardware part consists of a monitoring computer, a data transfer radio station, an uninterrupted power supply (UPS), and a display screen; and the software part includes a link communication protocol parse unit, a monitoring interface, and a guidance-model-based monitoring algorithm. According to the system, with a real-time location and tracking information, generated monitoring information containing the location and track and the like is calculated based on a guidance model, thereby solving a problem that no aerial vehicle location information and track information can not be obtained when the remote control and telemetering link of the unmanned aerial vehicle monitoring system is interrupted; a problem that a ground monitoring system displays wrong monitoring information because of an error occurring at unmanned aerial vehicle airborne system location information sending when the GPS positioning is out of operation during the blackout passing process can be solved; and functions that a wreckage falling point range can be predicted when the unmanned aerial vehicle crash happens and the like can be realized. The guidance-model-based fixed-wing unmanned aerial vehicle monitoring system has the broad application prospects in the field of the aircraft technology.


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    Title :

    Guidance-model-based fixed-wing unmanned aerial vehicle monitoring system


    Contributors:

    Publication date :

    2015-12-23


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    G08G Anlagen zur Steuerung, Regelung oder Überwachung des Verkehrs , TRAFFIC CONTROL SYSTEMS / H04L TRANSMISSION OF DIGITAL INFORMATION, e.g. TELEGRAPHIC COMMUNICATION , Übertragung digitaler Information, z.B. Telegrafieverkehr



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