The Proceedings of the Dynamics & Design Conference
Online ISSN : 2424-2993
2008
Session ID : 343
Conference information
343 Design of Intelligent Flight Control System for Unmanned Aerial Vehicles Considering Fault-Tolerance
Yuta KOBAYASHIMasaki TAKAHASHI
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Abstract
This research aims at proposing an intelligent flight control system which makes unmanned aerial vehicles tolerant of actuator faults. To make the unmanned system downsizing and low-cost, this study focuses on keeping the redundancy by software approach. The purpose of this study is to establish the systematic learning-based design method of control system with the evaluation function based on control purpose. The proposed technique adds to normal flight control system with detection, identification, and accommodation mechanisms. Each mechanism consists of neural network. In this study, the availability of the proposed system is verified by six-degree-of-freedom nonlinear simulation.
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© 2008 The Japan Society of Mechanical Engineers
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