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Before #14212 the velocity control gains used in the multicopter position controller were defined as a scale between velocity error in one axis (or it's integral and derivative respectively) and the unit thrust vector. The problem with this is that the normalization of the unit thrust vector changes per vehicle or even vehicle configuration as 0 and 100% thrust get a different physical response. That's why the gains are now defined as scale between velocity error (integral/derivative) and the output acceleration in m/s².