</action> <action dev="luc" type="add" > Added a utility method to compute Stirling numbers of the second kind. </action> <action dev="luc" type="add" > Added a new package dealing with differentials, for one or more free parameters and derivation order 1 or higher. </action> <...
In the Equation (4), J is the inertia matrix, M a t b is the resultant moment of the aerodynamic and thrust moments of the UAV, which is a nonlinear function of w n b b , v U A V b , and u 2 = [ ϖ a ϖ e ϖ r ] Τ is the control input of the rotation loop...