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March 10, 2020, 08:05 |
Coning motion of an aircraft
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#1 |
Senior Member
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Dear Foamers;
In solid body motion, rotating motion I am trying to create a coning motion of an aircraft. There are three omegas , Code:
\omega_x, \omega_y, \omega_z So far I what I have done : Code:
scalar t = time_.value(); // Rotation around axis scalar angleX = omegaX_->integrate(0, t); scalar angleY = omegaY_->integrate(0, t); scalar angleZ =omegaZ_->integrate(0, t); quaternion R1(axisX_, angleX); quaternion R2(axisY_, angleY); quaternion R3(axisZ_, angleZ); quaternion R = (R1*R2*R3); septernion TR(septernion(-origin_)*(R)*septernion(origin_)); |
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