How to calculate the roll-pitch-yaw of a given plane
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Dear everybody,
I have a plane whose equation is known (for example: ax+by+cz+d=0). Is it possible the calculate the roll-pitch-yaw angles of this plane?
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michael
2016년 10월 5일
just assume that one of the x,y,z is 0 in order to calculate the angles.
For example, for theta, which is the angle between x and y you can assume z=0 (it will be same result for any value of z, but for z=0 it is simplest). In this case, theta is the pitch.
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