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