I'm usually an excel ninja but this is kicking my butt.
I'm trying to make an excel lunar transfer dV calculator using equations from this website:
hthttp://www.braeunig.us/space/orbmech.htm#maneuver
I'm tring to turn equation 4.64 (eccentric anomaly) into an excel formula:
using the numbers from practice problem 4.18, here is what I'm puting into excel (raw number substisuted fro cell references):
=ATAN(POWER(1-POWER(D15,2),0.5)*SIN(157.7)/(D15+COS(157.7)))
instead of the desired 2.11 radians, I excel gives me .224
Any one know where I'm going wrong?
I'm trying to make an excel lunar transfer dV calculator using equations from this website:
hthttp://www.braeunig.us/space/orbmech.htm#maneuver
I'm tring to turn equation 4.64 (eccentric anomaly) into an excel formula:
using the numbers from practice problem 4.18, here is what I'm puting into excel (raw number substisuted fro cell references):
=ATAN(POWER(1-POWER(D15,2),0.5)*SIN(157.7)/(D15+COS(157.7)))
instead of the desired 2.11 radians, I excel gives me .224
Any one know where I'm going wrong?