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Fixed wing UAV navigation and control through integrated GNSS and vision精品.pdf

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Fixed wing UAV navigation and control through integrated GNSS and vision精品

AIAA Guidance, Navigation, and Control Conference and Exhibit AIAA 2005-5867 15 - 18 August 2005, San Francisco, California Fixed Wing UAV Navigation and Control through Integrated GNSS and Vision * † Mr. Peter J. Roberts and Dr Rodney A. Walker Airborne Avionics Research Group, Cooperative Research Centre for Satellite Systems, Queensland University of Technology, Brisbane, Australia and Peter O’Shea ‡ School of Electrical and Electronic Systems Engineering, Queensland University of Technology, Brisbane, Australia With the rapid deployment of Unmanned Airborne Vehicles (UAVs) into new applications, the pressure to extend the capabilities of current platforms is increasing. Increased capabilities, however, should preferably not come at the cost of increased aircraft size. In order to strive towards a more capable platform, the UAV must become increasingly aware of its current state (control, navigation and health) and surroundings (location of other aircraft, airspace boundaries, weather and terrain). This paper reports on the results of research into providing a new level of situational awareness to the UAV that is low in cost