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72results about "Simultaneous traffic control systems" patented technology

Child-mother type robot cooperation system of combination of unmanned surface vessel and unmanned aerial vehicle

The invention discloses a child-mother type robot cooperation system of combination of an unmanned surface vessel and an unmanned aerial vehicle. The child-mother type robot cooperation system comprises the unmanned surface vessel, the unmanned aerial vehicle and a ground station. The unmanned surface vessel comprises a vessel-mounted monitoring system. The unmanned aerial vehicle comprises an airborne monitoring system. The child-mother type robot system is formed by the unmanned surface vessel and the unmanned aerial vehicle. Besides, an unmanned aerial vehicle ground station monitoring system and an unmanned surface vessel ground station monitoring system are respectively arranged in a ground station monitoring system, and cooperative work between the unmanned surface vessel and the unmanned aerial vehicle is realized by information interaction between the two systems on the ground station. In cooperation of the unmanned surface vessel and the unmanned aerial vehicle, endurance of the unmanned aerial vehicle can be enhanced by the unmanned surface vessel, and the flight radius of the unmanned aerial vehicle can be extended; and more comprehensive observation perspectives and observation information can be provided for the unmanned surface vessel by the unmanned aerial vehicle.
Owner:范云生

Flight management system and method for providing navigational reference to emergency landing locations

An aviation navigational system and method for predicting glide range for an aircraft for specific airports and other potential emergency landing locations in proximity to the aircraft. Information is presented to the pilot by complementing a conventional moving map display with symbols centered on each landing location. GPS altitude, airport elevation, and the aircraft's glide ratio are factored into an equation to determine glide range for each airport within proximity to the aircraft. A circular symbol representing the glide range boundary is displayed around each airport. Each circular symbol represents a sectional view of an imaginary inverted cone, having the apex thereof centered on a given landing location. The size and shape of the cone is based on the gliding performance of the aircraft and the altitude differential between the aircraft and the target landing location. As the altitude differential increases the radius of the circle increases. Conversely as the altitude differential decreases, the radius of the circle decreases. As long as the aircraft is anywhere within any one of the three-dimensional inverted cones displayed, as represented by one or more circles on a two dimensional display, it can safely glide to the landing location. This display concept is selectively referred to herein as “cones of safety.”
Owner:CONTROL VISION CORP
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