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\be \begin{array}{l}\frac{d\mathbf{V}_f}{dt}= - \frac{C_{Daf} S_f \rho \mathbf{V}_f^2}{2 m_f}-g\sin\gamma_f\\\frac{d \gamma_f}{dt}=\frac{1}{\mathbf{V}_f} \left( \frac{C_{Laf}S_f\rho\mathbf{V}_{f}^2}{2m_f} -g\cos\gamma_f \right) \\\frac{dx}{dt}=V_f\cos\gamma_f \\\frac{dz}{dt}=V_f\sin\gamma_f\\\frac{d x_1}{dt}=V_s-V_f\cos\gamma_f\\\frac{d\theta_f}{dt}=\omega_{yf}\\\frac{d\omega_{yf}}{dt}=\frac{C_{mf}S_f l_f \rho \mathbf{V}_f^2}{2I_{yf}}\\\alpha_f=\theta_f-\gamma_f\end{array} \label{eq:rownruchsym}\ee \nsz
\documentclass[11pt,onecolumn,twoside,openright,b5paper]{mwbk}