Hi,
It looks like you're right, it should be fixed in master now.
Gautier
Le 16/10/2015 22:56, Sreenath Dama a écrit :
Hi,
In the function "get_vertical_thrust_coef" defined in "rotorcraft/guidance/guidance_v.c " . 30 deg has been compared with the last entry of rotation matrix att->m[8]. But last entry[i.e 9th entry] in the rotation matrix is Cos(X), where X is the angle between the gravity vector and thrust vector.
Is last entry of rotation matrix is intended to compare wth cos(30deg) instead of 30deg ?
Thanks,srinath
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