An approximate backstepping based trajectory tracking control of a gun launched micro aerial vehicle
Résumé
This paper considers the question of obtaining a nonlinear trajectory tracking control law for a comprehensive design of a Gun Launched Micro Aerial Vehicle - GLMAV. First, a nonlinear mathematical model of the GLMAV is presented for hover and near hover flight conditions. Then, an approximate backstepping control law is derived, allowing the trajectory tracking and the stabilization of the vehicleís position and orientation. Finally, numerical simulations are used to demonstrate the control law's good performance.