Variable-Structure Near-Space Vehicles with Time-Varying State Constraints Attitude Control Based on Switched Nonlinear System
This study is concerned with the attitude control problem of variable-structure near-space vehicles (VSNSVs) with time-varying state constraints based on switched nonlinear system. The full states of vehicles are constrained in the bounded sets with asymmetric time-varying boundaries. Firstly, consi...
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doaj-c363013a3fb144548699a1a5b36bd9c02020-11-25T01:27:38ZengMDPI AGSensors1424-82202020-02-0120384810.3390/s20030848s20030848Variable-Structure Near-Space Vehicles with Time-Varying State Constraints Attitude Control Based on Switched Nonlinear SystemCong Feng0Qing Wang1Chen Liu2Changhua Hu3Xiaohui Liang4Department of Automation Science and Electrical Engineering, Beihang University, Beijing 100191, ChinaDepartment of Automation Science and Electrical Engineering, Beihang University, Beijing 100191, ChinaScience and Technology on Special System Simulation Laboratory, Beijing Simulation Center, Beijing 100854, ChinaDepartment of Automation, High-Tech Institute of Xi’an, Xi’an 710000, ChinaDepartment of Automation Science and Electrical Engineering, Beihang University, Beijing 100191, ChinaThis study is concerned with the attitude control problem of variable-structure near-space vehicles (VSNSVs) with time-varying state constraints based on switched nonlinear system. The full states of vehicles are constrained in the bounded sets with asymmetric time-varying boundaries. Firstly, considering modeling uncertainties and external disturbances, an extended state observer (ESO), including two distinct linear regions, is proposed with the advantage of avoiding the peaking value problem. The disturbance observer is utilized to estimate the total disturbances of the attitude angle and angular rate subsystems, which are described in switched nonlinear systems. Then, based on the estimation values, the asymmetric time-varying barrier Lyapunov function (BLF) is employed to construct the active disturbance rejection controller, which can ensure the full state constraints are not violated. Furthermore, to resolve the ‘explosion of complexity’ problem in backstepping control, a modified dynamic surface control is proposed. Rigorous stability analysis is given to prove that all signals of the closed-loop system are bounded. Numerical simulations are carried out to demonstrate the effectiveness of the proposed control scheme.https://www.mdpi.com/1424-8220/20/3/848time-varying state constraintsactive disturbance rejection controlvariable structure near space vehicledynamic surface controlswitched nonlinear system |
collection |
DOAJ |
language |
English |
format |
Article |
sources |
DOAJ |
author |
Cong Feng Qing Wang Chen Liu Changhua Hu Xiaohui Liang |
spellingShingle |
Cong Feng Qing Wang Chen Liu Changhua Hu Xiaohui Liang Variable-Structure Near-Space Vehicles with Time-Varying State Constraints Attitude Control Based on Switched Nonlinear System Sensors time-varying state constraints active disturbance rejection control variable structure near space vehicle dynamic surface control switched nonlinear system |
author_facet |
Cong Feng Qing Wang Chen Liu Changhua Hu Xiaohui Liang |
author_sort |
Cong Feng |
title |
Variable-Structure Near-Space Vehicles with Time-Varying State Constraints Attitude Control Based on Switched Nonlinear System |
title_short |
Variable-Structure Near-Space Vehicles with Time-Varying State Constraints Attitude Control Based on Switched Nonlinear System |
title_full |
Variable-Structure Near-Space Vehicles with Time-Varying State Constraints Attitude Control Based on Switched Nonlinear System |
title_fullStr |
Variable-Structure Near-Space Vehicles with Time-Varying State Constraints Attitude Control Based on Switched Nonlinear System |
title_full_unstemmed |
Variable-Structure Near-Space Vehicles with Time-Varying State Constraints Attitude Control Based on Switched Nonlinear System |
title_sort |
variable-structure near-space vehicles with time-varying state constraints attitude control based on switched nonlinear system |
publisher |
MDPI AG |
series |
Sensors |
issn |
1424-8220 |
publishDate |
2020-02-01 |
description |
This study is concerned with the attitude control problem of variable-structure near-space vehicles (VSNSVs) with time-varying state constraints based on switched nonlinear system. The full states of vehicles are constrained in the bounded sets with asymmetric time-varying boundaries. Firstly, considering modeling uncertainties and external disturbances, an extended state observer (ESO), including two distinct linear regions, is proposed with the advantage of avoiding the peaking value problem. The disturbance observer is utilized to estimate the total disturbances of the attitude angle and angular rate subsystems, which are described in switched nonlinear systems. Then, based on the estimation values, the asymmetric time-varying barrier Lyapunov function (BLF) is employed to construct the active disturbance rejection controller, which can ensure the full state constraints are not violated. Furthermore, to resolve the ‘explosion of complexity’ problem in backstepping control, a modified dynamic surface control is proposed. Rigorous stability analysis is given to prove that all signals of the closed-loop system are bounded. Numerical simulations are carried out to demonstrate the effectiveness of the proposed control scheme. |
topic |
time-varying state constraints active disturbance rejection control variable structure near space vehicle dynamic surface control switched nonlinear system |
url |
https://www.mdpi.com/1424-8220/20/3/848 |
work_keys_str_mv |
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