Adaptive controler of Major function for controlling elastic aerial vehicle
Adaptive controler of Major function for controlling elastic aerial vehicle
An adaptive controller of the major function for an aerial vehicle's (AV) longitudinal motion with account for the wing aeroelasticity is discussed in this research. A nonlinear mathematical model of resilient aircraft's longitudinal motion is designed. Adaptive control system of a resilient AV is built by means of majorizing function and its efficiency is tested under the uncertainty parameter function of AV model.