Integrated design of missile guidance and control: Active disturbance rejection control method

Abstract

In this paper, we present an active disturbance rejection control (ADRC) based integrated guidance and control (IGC) law. The IGC law is designed using the backstepping technique, and the particle swarm optimization (PSO) algorithm is utilized to find the optimal selection of the controller parameters. Simulation results show that, with the application of… (More)

Topics

5 Figures and Tables

Slides referencing similar topics