Convert lift, drag and side into body axis?
Posted: Tue Oct 25, 2016 5:46 pm
https://forum.flightgear.org/search.php ... 43510df09e
Calculate the resultant and from this use the cos and sine of the wings incidence to the fuselage body to find the x and z values.
Calculate the resultant and from this use the cos and sine of the wings incidence to the fuselage body to find the x and z values.