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![]() "d&tm" wrote in message ... "Chad Speer" wrote in message oups.com... Terry - thanks for the reply, but heading is not known. Stefan - we need to be able to plug these known values into a formula and kick out a result. Assuming the original responder was on the right track, I still don't know what to do with his suggestion. Any ideas on that? I'm not lazy, this just went over my head a long time ago. :-) Chad, sorry misread the question. But I like a challenge so I had another go. Firstly I dont believe the equations given by the original poster are correct. if you apply the cosine rule to the wind triangle for 2 aircraft you get the following 2 equations. TAS1^2=WS^2+GS1^2-2WSGS1COS(180-ABS(WD-TR1) TAS2^2=WS^2+GS2^2-2WSGS2COS(180-ABS(WD-TR2) WHERE TAS1 AND TAS2 ARE TRUE AIRSPEEDS FOR AIRCRAFT 1 AND 2 WS = WIND SPEED WD =WIND DIRECTION IN DEGREES MAG TR1 AND TR2 ARE TRACKS MAGNETIC FOR AIRCRAFT 1 AND 2 GS1 AND GS2 ARE GROUND SPEEDS FOR AIRCRAFT 1 AND 2. (180-ABS(WD-TR) WILL GIVE YOU THE ACTUAL ANGLE BETWEEN WIND DIRECTION AND TRACK. Further to this post ,using the above 2 equations , with the following correction cos( abs( abs(wd -tr)-180)), the problem was solved graphically by solving the 2 quadratics , or 3 for a 3 aircraft case for wind speed, for each of the 360 degrees of possible wind direction. this gives you a parabola for each aircraft and the overlap of the parablolas gives you the required answer. For 2 aircraft there can be either 1 or 2 solutions. having a 3rd aircraft will give one unique solution.. This solution is available as an Excel spreadsheet if anybody is interested. terry |
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