Abstract:
In this article, the proposed method first evaluates the effects on aerodynamic force caused by flight velocity and angular velocity of the parafoil delivery system and p...Show MoreMetadata
Abstract:
In this article, the proposed method first evaluates the effects on aerodynamic force caused by flight velocity and angular velocity of the parafoil delivery system and performs an active disturbance rejection control in the horizontal direction. Moreover, a glide-ratio controller is designed based on the characteristics of the symmetrical flap deflection. For resisting its disturbance, a feedforward compensation unit is designed with the glide-ratio controller. The performance is effectively validated through hardware-in-the-loop simulation.
Published in: IEEE Transactions on Aerospace and Electronic Systems ( Volume: 56, Issue: 3, June 2020)