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In article ,
Andy Blackburn wrote: What if, in instances where we are using a 1 mile cylinder for the finish, instead of putting in a hard deck of 500', we make it so the scoring program can calculate TOTAL ENERGY for each glider at the one mile point (this should be relatively easy to do). The idea would be for each sailplane to have at least 500' of EQUIVALENT ALTITUDE at 1 mile. That is, take actual AGL altitude and add the equivalent altitude that the glider would have if it's kinetic energy were converted to altitude (at say 60 knots). I agree with the idea, but the fly in the ointment is wind -- the analysis computer won't know what the wind is, so it can only know your groundspeed not your airspeed. It will thus let you get away with a lower airspeed if you're going downwind, while you'll need a higher airspeed to satisfy it if you're going upwind. Fortunately, these errors are in the sensible direction, but the magnitudes of them may or may not be sensible. -- Bruce |
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