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Table 2.

Non-dimensional control derivatives

\(X_{{\Phi}}^{+}\)
\(Z_{{\Phi}}^{+}\)
\(M_{{\Phi}}^{+}\)
\(X_{{\alpha}1}^{+}\)
\(Z_{{\alpha}1}^{+}\)
\(M_{{\alpha}1}^{+}\)
\(X_{{\bar{{\phi}}}}^{+}\)
\(Z_{{\bar{{\phi}}}}^{+}\)
\(M_{{\bar{{\phi}}}}^{+}\)
\(X_{{\alpha}2}^{+}\)
\(Z_{{\alpha}2}^{+}\)
\(M_{{\alpha}2}^{+}\)
–2.06 0.03 0.04 –2.91 0.03 –0.19 –3.58 –3.08 0.01 0.53 
\(X_{{\Phi}}^{+}\)
\(Z_{{\Phi}}^{+}\)
\(M_{{\Phi}}^{+}\)
\(X_{{\alpha}1}^{+}\)
\(Z_{{\alpha}1}^{+}\)
\(M_{{\alpha}1}^{+}\)
\(X_{{\bar{{\phi}}}}^{+}\)
\(Z_{{\bar{{\phi}}}}^{+}\)
\(M_{{\bar{{\phi}}}}^{+}\)
\(X_{{\alpha}2}^{+}\)
\(Z_{{\alpha}2}^{+}\)
\(M_{{\alpha}2}^{+}\)
–2.06 0.03 0.04 –2.91 0.03 –0.19 –3.58 –3.08 0.01 0.53 

\(X_{{\Phi}}^{+}\)
⁠,
\(Z_{{\Phi}}^{+}\)
and
\(M_{{\Phi}}^{+}\)
, non-dimensional derivatives of the x- and z-component of the aerodynamic force and aerodynamic moment, respectively, with respect to the Φ;
\(X_{{\alpha}1}^{+}\)
,
\(Z_{{\alpha}1}^{+}\)
and
\(M_{{\alpha}1}^{+}\)
, non-dimensional derivatives of the x- and z-component of the aerodynamic force and aerodynamic moment, respectively, with respect to α1;
\(X_{{\bar{{\phi}}}}^{+}\)
,
\(Z_{{\bar{{\phi}}}}^{+}\)
and
\(M_{{\bar{{\phi}}}}^{+}\)
,non-dimensional derivatives of the x- and z-component of the aerodynamic force and aerodynamic moment, respectively, with respect to the
\({\bar{{\phi}}}\)
;
\(X_{{\alpha}2}^{+}\)
,
\(Z_{{\alpha}2}^{+}\)
and
\(M_{{\alpha}2}^{+}\)
, non-dimensional derivatives of the x- and z-component of the aerodynamic force and aerodynamic moment, respectively, with respect to α2

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