... for optimizing control characteristics in novel aircraft configurations. Redundancy in control surfaces: The proposed design incorporates dual elevons to enhance control allocation and stability, addressing challenges posed by the absence of a traditional tail. This redundancy in control surfaces improves...

... improve significantly. This is especially important for a safe and stable transition from rotary-wing to fixed-wing flight, which should be done quickly. The authors also propose a control allocation strategy with MPC algorithm to exploit the thrust and control inputs of both rotary-wing and fixed-wing...

... only Disturbance observer Barrier Lyapunov function Control allocation Gust response stabilization Sliding mode differentiator Assumption 3: The true airspeed has been regulated or controlled by the throttle lever or engine power lever. So, in the following definition and design...

... with multi‐input and multi‐output, the control system design includes a control allocator, a dynamic inversion controller and two PID controllers. The control allocator is designed based on pseudo inverse method; the dynamic inversion controller is applied to make the original system decoupled into two...