DocumentCode :
1941315
Title :
Comparison of Real-time Online and Offline Neural Network Models for a UAV
Author :
Puttige, Vishwas R. ; Anavatti, Sreenatha G.
Author_Institution :
Australian Defence Force Acad., Canberra
fYear :
2007
fDate :
12-17 Aug. 2007
Firstpage :
412
Lastpage :
417
Abstract :
In this paper a comparison of an offline and online neural network architecture for the identification of an unmanned aerial vehicle (UAV) is presented. The identification algorithm is based on autoregressive model aided by neural networks for the six degree of freedom, non-linear dynamics of a fixed wing UAV. One of the architectures involved the use of a single network to model the complete UAV system and the other involved the use of two decoupled networks for the lateral and longitudinal dynamics taking coupling into account. Numerical simulation results are presented for each of these architectures. The results have been validated using the real-time hardware in the loop (HIL) simulation technique for different sets of flight data.
Keywords :
aerospace robotics; aircraft control; autoregressive processes; mobile robots; neural net architecture; neurocontrollers; nonlinear control systems; remotely operated vehicles; robot dynamics; autoregressive model; decoupled networks; hardware in the loop simulation; lateral dynamics; longitudinal dynamics; nonlinear dynamics; numerical simulation; offline neural network architecture; online neural network architecture; six degree of freedom; unmanned aerial vehicle; Aerodynamics; Aerospace control; Artificial neural networks; Biological neural networks; Military aircraft; Neural networks; Nonlinear dynamical systems; System identification; Unmanned aerial vehicles; Vehicle dynamics;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Neural Networks, 2007. IJCNN 2007. International Joint Conference on
Conference_Location :
Orlando, FL
ISSN :
1098-7576
Print_ISBN :
978-1-4244-1379-9
Electronic_ISBN :
1098-7576
Type :
conf
DOI :
10.1109/IJCNN.2007.4370992
Filename :
4370992
Link To Document :
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