среда, 23 декабря 2009 г.

94

Now type: « MR2 COS * 7699.0 ENT M1 407.9 / MR1 ENT M1 » (Result stored in M1)
And continue:
« MR2 TAN – MR1 ENT SPEC ATAN »
Final Accurate Launch Azimuth = 42.8491°
So, the complete DGIV calculator formula is as follow:
YourLat = Actual latitude
DesInc = Wanted inclinaison
FinalSpeed = Target Orbital speed
Actual Speed = Actual speed (due to planet rotation)
« YourLat COS M1 DesInc COS / MR1 ENT SPEC ASIN M2 MR2 COS * FinalSpeed ENT M1 ActualSpeed /
MR1 ENT M1 MR2 TAN – MR1 ENT SPEC ATAN »

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