Practical experience of intellectual uav attitude stabilization system computer-aided design

Practical experience of intellectual uav attitude stabilization system computer-aided design

A. A. Tunik, К. Rydlo, O. V Savchenko, K. V. Melnik

 

Abstract

The problem of design of the intellectual attitude control system for small UAV is considered.This system is designated for UAV stability and controllability augmentation in the manual control mode. This problem is solved via combination of the traditional and robust control, and usage of the model-oriented design approach. The results of design are verified in the processes of multi-stage simulationand experimental flight tests; their interpretation is given

Keywords

UAV; Stability and Controllability Augmentation System; attitude determination; attitude control; robust control; simulation; flight test

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