DocumentCode :
1798046
Title :
Non-singular Terminal sliding mode control for landing on asteroids based on RBF neural network
Author :
Liu, K.P. ; Liu, F.X. ; Liu, S.S. ; Li, Y.C.
Author_Institution :
Coll. of Electr. & Electron. Eng., Changchun Univ. of Technol., Changchun, China
fYear :
2014
fDate :
6-11 July 2014
Firstpage :
1291
Lastpage :
1295
Abstract :
A method of non-singular Terminal sliding mode control was proposed for landing asteroids with uncertainty and strong nonlinearity based on RBF neural network. The dynamics of the detector in the landing environment was analyzed, and the nominal trajectory guidance method based on optimal polynomial was designed, by which the consumption of fuel was suboptimal. Controller was designed using non-singular Terminal sliding mode. The influences caused by unknown disturbance and uncertainty during landing phase was compensated by RBF neural network real-time compensation, which could effectively suppress the influence of external disturbance and weaken the system chattering. Simulation results show that the proposed method was effective.
Keywords :
aircraft landing guidance; asteroids; compensation; control nonlinearities; control system synthesis; neurocontrollers; polynomials; radial basis function networks; trajectory control; uncertain systems; variable structure systems; RBF neural network real-time compensation; asteroid landing; detector dynamics; external disturbance influence suppression; fuel consumption; nominal trajectory guidance method; nonsingular terminal sliding mode control method; optimal polynomial; strong nonlinearity; system chattering; uncertainty; unknown disturbance; Acceleration; Detectors; Neural networks; Probes; Sliding mode control; Trajectory; Vectors;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Neural Networks (IJCNN), 2014 International Joint Conference on
Conference_Location :
Beijing
Print_ISBN :
978-1-4799-6627-1
Type :
conf
DOI :
10.1109/IJCNN.2014.6889747
Filename :
6889747
Link To Document :
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