DocumentCode
3510214
Title
Simulation of Dynamic Inversion with Neural Network and its Applications to MAV
Author
He Guang-Lin ; Wu Guo-hui
Author_Institution
Sch. of Aerosp. Sci. & Technol., Beijing Inst. of Technol., Beijing
fYear
2008
fDate
1-3 Nov. 2008
Firstpage
60
Lastpage
63
Abstract
The MAV accurate modes are typically unavailable. Most traditional methods for system design are complex and can not get satisfactory effect. Recent work in dynamic inversion with neural network may be applied to control a MAV where the reference commands include position, velocity, attitude and angular rate. This control technology can provide the MAV with an admirably command follow and steady control capability. Neural networks are used directly as the controller as well as indirect designs that are based on a neural network process model. The emulator is compiled by using NNCTRL20 and NNSYSID20 in MATLAB. Then the main result of this simulation is presented. It indicates that the method has high precision and strong stability, which can serve the control of MAV. Thereafter, an amendment about controlling system with dynamic inversion of the MAV is described.
Keywords
aircraft control; neurocontrollers; stability; MATLAB; MAV; NNCTRL20; NNSYSID20; dynamic inversion; neural network; steady control capability; Aerodynamics; Aerospace control; Aircraft; Algorithm design and analysis; Attitude control; Control systems; Intelligent networks; Mathematical model; Neural networks; Nonlinear dynamical systems; MATLAB; MAV; dynamic inversion; neural network;
fLanguage
English
Publisher
ieee
Conference_Titel
Intelligent Networks and Intelligent Systems, 2008. ICINIS '08. First International Conference on
Conference_Location
Wuhan
Print_ISBN
978-0-7695-3391-9
Electronic_ISBN
978-0-7695-3391-9
Type
conf
DOI
10.1109/ICINIS.2008.56
Filename
4683168
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