Stochastic simulation of the automatic control systems of unmanned aircraft using optimal Kalman filter

Abstract

Сlosed loop continuous and discrete automatic control systems of unmanned aircraft which contain the autopilot, the glider, sensors and Kalman filters in a straight chain are considered. Discrete model of the system and present in graphs simulation results is proposed.

Keywords

• системы автоматического управления
• фильтр калмана
• устойчивость систем