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At 38:00, shouldn't gamma be the ratio coefficient of moment divided by coefficient of drag?
can you show how to implement on simulink?
I have Doubt regarding the way you have derived U2! , (p,q,r ) are in body frame, whereas ( phi_dot, theta_dot, psi_dot) are in inertial frame. Shouldn't be the equation for control law for U2 be in terms of (phi_dot, theta_dot, psi_dot)?
thank you so much. bro
Thank you so much Sir Ji 🙏🙏🙏🙏🙏
Thank you sir, you might've just saved my project
At 38:00, shouldn't gamma be the ratio coefficient of moment divided by coefficient of drag?
can you show how to implement on simulink?
I have Doubt regarding the way you have derived U2! , (p,q,r ) are in body frame, whereas ( phi_dot, theta_dot, psi_dot) are in inertial frame. Shouldn't be the equation for control law for U2 be in terms of (phi_dot, theta_dot, psi_dot)?
thank you so much. bro
Thank you so much Sir Ji 🙏🙏🙏🙏🙏
Thank you sir, you might've just saved my project