Title
Neural Adaptive Integral Sliding Mode Control For Attitude Tracking Of Flexible Spacecraft With Signal Quantisation And Actuator Nonlinearity
Abstract
This study investigates the neural adaptive integral sliding mode control for attitude tracking of flexible spacecraft, where unknown actuator nonlinearity, input quantisation and external disturbances are considered simultaneously. In this design, the hysteresis encoder-decoder scheme is employed between the controller and actuator side for signal quantisation. A quantised adaptive integral sliding mode control strategy is developed, where the neural network scheme is applied to approximate the unmeasurable rigid-flexible coupled nonlinear dynamics. The proposed control strategy can compensate for quantisation error, actuator faults, actuator dead-zone as well as external disturbances effectively, and guarantee the trajectory of the attitude tracking error converge to the equilibrium point along the designed sliding surface. Finally, a simulation example is conducted to demonstrate the validness of the developed quantised control strategy for flexible spacecraft attitude tracking problem.
Year
DOI
Venue
2020
10.1080/00207721.2020.1803441
INTERNATIONAL JOURNAL OF SYSTEMS SCIENCE
Keywords
DocType
Volume
Flexible spacecraft control, attitude tracking control, adaptive integral sliding mode control, input quantisation, unknown actuator deadzone, actuator fault
Journal
51
Issue
ISSN
Citations 
15
0020-7721
0
PageRank 
References 
Authors
0.34
0
3
Name
Order
Citations
PageRank
Qiuhong Liu1222.98
Ming Liu2393.54
Yan Shi36012.08