Airship spatial motion control based on the analytical design of aggregated adjuster method

Abstract

A dynamic model of the airship is developed. The problem of controlling the airship spatial movement during take off and cruising flight is solved. Based on the method of analytical design of aggregated adjuster (ADAA) method, a vector control is synthesized that ensures the convergence of the motion to the desired manifolds. An analysis of the stability of a closed control system was carried out. The efficiency of the algorithm by mathematical modeling is proven. Keywords airship, takeoff, cruising, ADAA, manifolds, stability