forked from Archive/PX4-Autopilot
correctin from user input to roll and pitch
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@ -2161,7 +2161,7 @@ MulticopterPositionControl::task_main()
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// use the formula z_roll_pitch_sp = R_tilt * [0;0;1]
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// R_tilt is computed from_euler; only true if cos(roll) not equal zero
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// -> valid if roll is not +-pi/2
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// -> valid if roll is not +-pi/2;
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_att_sp.roll_body = -asinf(z_roll_pitch_sp(1));
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_att_sp.pitch_body = atan2f(z_roll_pitch_sp(0), z_roll_pitch_sp(2));
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