An update algorithm design using moving Region of Attraction for SDRE based control law

被引:9
作者
Copur, Engin H. [1 ]
Arican, Ahmet C. [2 ]
Ozcan, Sinan [3 ]
Salamci, Metin U. [2 ]
机构
[1] Necmettin Erbakan Univ, Dept Space & Satellite Engn, TR-42090 Konya, Turkey
[2] Gazi Univ, Dept Mech Engn, TR-06570 Ankara, Turkey
[3] Turkish Aerosp, TR-06980 Ankara, Turkey
来源
JOURNAL OF THE FRANKLIN INSTITUTE-ENGINEERING AND APPLIED MATHEMATICS | 2019年 / 356卷 / 15期
关键词
DEPENDENT RICCATI EQUATION; TRACKING CONTROL; STABILITY; SYSTEMS; HELICOPTER; SCHEME;
D O I
10.1016/j.jfranklin.2019.08.007
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
State Dependent Riccati Equation (SDRE) methods have the considerable advantages over other nonlinear control methods. However, stability issues can be arisen in SDRE based control system due to the lack of the global asymptotic stability property. Therefore, the previous studies have usually shown that local asymptotic stability can be ensured by estimating a Region of Attraction (ROA) around the equilibrium point. These estimated regions for stability may become narrow or the condition to keep the states in this region may be very conservative. To resolve these issues, this paper proposes a novel SDRE method employing an update algorithm to re-estimate the ROA when the states tend to move out of the stable region. The tendency is checked using a condition which is developed based on a new theorem. The theorem proves that it is possible to redesign the previous ROA with respect to the current states lying close to its boundary for ensuring the "non-local" stability along the trajectory without the need of solving SDRE at each time instant, unlike the standard SDRE approach. Therefore, the new theorem is now able to enhance the stability of the SDRE based closed-loop control system. The feasibility of the proposed SDRE control method is tested in both simulations and experiments. A validated 3-DOF laboratory helicopter is used for experiments and the control objective for the helicopter is to realise a preplanned movement in both elevation and travel axes. The results reveal that the proposed SDRE approach enables the controlled plant to track the desired trajectory as satisfactorily as the standard SDRE approach, while only solving SDRE when needed. The proposed SDRE method reduces the computational load for practical implementation of the control algorithm whilst ensuring the stability over the operational region. (C) 2019 The Franklin Institute. Published by Elsevier Ltd. All rights reserved.
引用
收藏
页码:8388 / 8413
页数:26
相关论文
共 46 条
[1]  
Anderson J. D., 1999, Aircraft Performance and Design
[2]  
[Anonymous], P 26 INT C INF COM A
[3]  
[Anonymous], 2014, IFAC P, DOI DOI 10.3182/20140824-6-ZA-1003.02282
[4]  
Arican AC, 2018, 2018 19TH INTERNATIONAL CARPATHIAN CONTROL CONFERENCE (ICCC), P185, DOI 10.1109/CarpathianCC.2018.8399625
[5]  
Babaei N., 2019, EUR J CONTROL
[6]   Personalized drug administration for cancer treatment using Model Reference Adaptive Control [J].
Babaei, Naser ;
Salamci, Metin U. .
JOURNAL OF THEORETICAL BIOLOGY, 2015, 371 :24-44
[7]   Output tracking control of uncertain nonlinear second-order systems [J].
Bartolini, G ;
Ferrara, A ;
Usai, E .
AUTOMATICA, 1997, 33 (12) :2203-2212
[8]   State-dependent Riccati equation control for small autonomous helicopters [J].
Bogdanov, Alexander ;
Wan, Eric .
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2007, 30 (01) :47-60
[9]   Continuous Differentiator Based on Adaptive Second-Order Sliding-Mode Control for a 3-DOF Helicopter [J].
Castaneda, Herman ;
Plestan, Franck ;
Chriette, Abdelhamid ;
de Leon-Morales, Jesus .
IEEE TRANSACTIONS ON INDUSTRIAL ELECTRONICS, 2016, 63 (09) :5786-5793
[10]   An Approach to Design Robust Tracking Controllers for Nonlinear Uncertain Systems [J].
Celentano, Laura ;
Basin, Michael V. .
IEEE TRANSACTIONS ON SYSTEMS MAN CYBERNETICS-SYSTEMS, 2020, 50 (08) :3010-3023