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Update examples
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@@ -147,11 +147,11 @@ void MulticopterAttitudeControlBase::control_attitude(float dt)
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if (e_R_z_cos < 0.0f) {
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/* for large thrust vector rotations use another rotation method:
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* calculate angle and axis for R -> R_sp rotation directly */
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math::Quaternion q;
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q.from_dcm(R.transposed() * R_sp);
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math::Vector <3> e_R_d = q.imag();
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math::Quaternion ql;
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ql.from_dcm(R.transposed() * R_sp);
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math::Vector <3> e_R_d = ql.imag();
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e_R_d.normalize();
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e_R_d *= 2.0f * atan2f(e_R_d.length(), q(0));
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e_R_d *= 2.0f * atan2f(e_R_d.length(), ql(0));
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/* use fusion of Z axis based rotation and direct rotation */
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float direct_w = e_R_z_cos * e_R_z_cos * yaw_w;
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