A system for graphically displaying on a cockpit display an indication of closure (i.e. a "closure indictor") with a selected target aircraft. In a preferred embodiment of the invention, the system only displays a closure indicator if: (1) the selected target aircraft is within a pre-determined monitoring zone; and (2) the track of the selected target aircraft is within a pre-determined variation angle of the track of the Own Ship aircraft. If the rate of closure between the selected target aircraft and the Own Ship aircraft is within a predetermined range of values, the closure indicator includes a closing/receding indicia (such as an upwardly or downwardly directed arrow) that indicates whether the Own Ship aircraft is closing in on or receding from the selected target aircraft. The system preferably removes the closure indicator from display when the Own Ship aircraft or the selected target aircraft ceases to be airborne.

 
Web www.patentalert.com

< Drain particularly for engine support strut

< Multi-junction photovoltaic cell having buffer layers for the growth of single crystal boron compounds

> Relative attitude estimator for multi-payload attitude determination

> System and apparatus for propelling and carrying a user within a confined interior

~ 00295