Switching disturbance rejection attitude control of near space vehicles with variable structure

doi:10.21629/JSEE.2019.01.16

Journal of Systems Engineering and Electronics ›› 2019, Vol. 30 ›› Issue (1): 167-179.doi: 10.21629/JSEE.2019.01.16

收稿日期:2017-08-18 出版日期:2019-02-27 发布日期:2019-02-27

Switching disturbance rejection attitude control of near space vehicles with variable structure

Ligang GONG¹(), Qing WANG^1,*(), Chaoyang DONG²()

¹ School of Automation Science and Electrical Engineering, Beihang University, Beijing 100191, China
² School of Aeronautic Science and Engineering, Beihang University, Beijing 100191, China

Received:2017-08-18 Online:2019-02-27 Published:2019-02-27
Contact: Qing WANG E-mail:jackstrawberry@126.com;bhwangqing@126.com;bhdongchaoyang@126.com
About author:GONG Ligang was born in 1992. He received his B.S. degree in automatic control from Beihang University, Beijing, China, in 2013. He is currently a Ph.D. candidate in School of Automation Science and Electrical Engineering, Beihang University. His research interests include nonlinear systems, aircraft guidance and control and intelligence control. E-mail:jackstrawberry@126.com|WANG Qing was born in 1968. She received her Ph.D. degree in flight control, guidance and simulation from Northwestern Polytechnical University, Xi'an, China, in 1996. She is currently a professor in School of Automation Science and Electrical Engineering, Beihang University. Her research interests include missile guidance and control, switch control, and fault detection. E-mail:bhwangqing@126.com|DONG Chaoyang was born in 1966. He received his Ph.D. degree in guidance, navigation and control from Beihang University, Beijing, China, in 1996. He is currently a professor in School of Aeronautic Science and Engineering, Beihang University. His research interests include dynamics and control of flight vehicles, modeling and simulation of aerospace vehicles, and synthesis of aerospace electrical system. E-mail:bhdongchaoyang@126.com
Supported by:
the National Natural Science Foundation of China(61374012);the Aeronautical Science Foundation of China(2016ZA51011);This work was supported by the National Natural Science Foundation of China (61374012) and the Aeronautical Science Foundation of China (2016ZA51011)

摘要/Abstract

Abstract:

A switching disturbance rejection attitude control law is proposed for a near space vehicle (NSV) with variable structure. The multiple flight modes, system uncertainties and disturbances of the NSV are taken into account based on switched nonlinear systems. Compared with traditional backstepping design methods, the proposed method utilizes the added integrals of attitude angle and angular rate tracking errors to further decrease the tracking errors. Moreover, to reduce the computation complexity, a rapid convergent differentiator is employed to obtain the derivative of the virtual control command. Finally, for disturbance rejection, based on the idea from the extended state observer (ESO), two disturbance observers are designed by using non-smooth functions to estimate the disturbances in the switched nonlinear systems. All signals of the closed-loop system are proven to be uniformly ultimately bounded under the Lyapunov function framework. Simulation results demonstrate the effectiveness of the proposed control scheme.

Key words: near space vehicle (NSV), variable structure, switched nonlinear system, extended state observer (ESO)

. [J]. Journal of Systems Engineering and Electronics, 2019, 30(1): 167-179.

Ligang GONG, Qing WANG, Chaoyang DONG. Switching disturbance rejection attitude control of near space vehicles with variable structure[J]. Journal of Systems Engineering and Electronics, 2019, 30(1): 167-179.

图/表 12

参考文献 45

1	CHAI R, SAVVARIS A, TSOURDOS A, et al. Multi-objective trajectory optimization of space manoeuvre vehicle using adaptive differential evolution and modified game theory. Acta Astronautica, 2017, 136, 273- 280. doi: 10.1016/j.actaastro.2017.02.023
2	SZIROCZAK D, SMITH H. A review of design issues specific to hypersonic flight vehicles. Progress in Aerospace Sciences, 2016, 84, 1- 28. doi: 10.1016/j.paerosci.2016.04.001
3	QUADRELLI M B, WOOD L J, RIEDEL J E, et al. Guidance, navigation, and control technology assessment for future planetary science missions. Journal of Guidance, Control, and Dynamics, 2015, 38 (7): 1165- 1186. doi: 10.2514/1.G000525
4	VIVIANI A, IUSPA L, APROVITOLA A. An optimizationbased procedure for self-generation of re-entry vehicles shape. Aerospace Science and Technology, 2017, 68, 123- 134. doi: 10.1016/j.ast.2017.05.009
5	ALBISSER M, DOBRE S, BERNER C, et al. Aerodynamic coefficient identification of a space vehicle from multiple freeflight tests. Journal of Spacecraft and Rockets, 2017, 54 (2): 426- 435. doi: 10.2514/1.A33587
6	REN Z, FU W, YAN J, et al. Discrete reconfigurable backstepping attitude control of reentry hypersonic flight vehicle. Advances in Mechanical Engineering, 2017, 9 (4): 1- 13.
7	ZHANG J, SUN C, ZHANG R, et al. Adaptive sliding mode control for re-entry attitude of near space hypersonic vehicle based on backstepping design. IEEE/CAA Journal of Automatica Sinica, 2015, 2 (1): 94- 101. doi: 10.1109/JAS.2015.7032910
8	YAN X, CHEN M, WU Q, et al. Adaptive neural tracking control for near-space vehicles with stochastic disturbances. International Journal of Advanced Robotic Systems, 2017, 14 (3): 1- 9.
9	SHAO X, WANG H. Active disturbance rejection based trajectory linearization control for hypersonic reentry vehicle with bounded uncertainties. ISA Transactions, 2015, 54, 27- 38. doi: 10.1016/j.isatra.2014.06.010
10	ZHANG J, SUN T. Disturbance observer-based sliding manifold predictive control for reentry hypersonic vehicles with multi-constraint. Proc. of the Institution of Mechanical Engineers, Part G:Journal of Aerospace Engineering, 2016, 230 (3): 485- 495. doi: 10.1177/0954410015593564
11	CHANG Y, JIANG T, PU Z. Adaptive control of hypersonic vehicles based on characteristic models with fuzzy neural network estimators. Aerospace Science and Technology, 2017, 68, 475- 485. doi: 10.1016/j.ast.2017.05.043
12	ROSSMAN G, LE VINE M J, LAWLOR S, et al. Conceptual design of a small earth reentry vehicle for biological sample return. Journal of Spacecraft and Rockets, 2017, 54 (1): 246- 257. doi: 10.2514/1.A33568
13	AJAJ R M, BEAVERSTOCK C S, FRISWELL M I. Morphing aircraft:the need for a new design philosophy. Aerospace Science and Technology, 2016, 49, 154- 166. doi: 10.1016/j.ast.2015.11.039
14	JUNGERS R M, AHMADI A A, PARRILO P A, et al. A characterization of Lyapunov inequalities for stability of switched systems. IEEE Trans. on Automatic Control, 2017, 62 (6): 3062- 3067.
15	ZHANG D, SHI P, WANG Q G. Energy-efficient distributed control of large-scale systems:a switched system approach. International Journal of Robust and Nonlinear Control, 2016, 26 (14): 3101- 3117. doi: 10.1002/rnc.3494
16	LIN X, CHEN C C, QIAN C. Smooth output feedback stabilization of a class of planar switched nonlinear systems under arbitrary switchings. Automatica, 2017, 82, 314- 318. doi: 10.1016/j.automatica.2017.03.020
17	LIU Z, CHEN B, LIN C. Adaptive neural backstepping for a class of switched nonlinear system without strict-feedback form. IEEE Trans. on Systems, Man, and Cybernetics:Systems, 2017, 47 (7): 1315- 1320. doi: 10.1109/TSMC.2016.2585664
18	LI Y, TONG S, LIU L, et al. Adaptive output-feedback control design with prescribed performance for switched nonlinear systems. Automatica, 2017, 80, 225- 231. doi: 10.1016/j.automatica.2017.02.005
19	ZHAO X, YIN Y, ZHANG L, et al. Control of switched nonlinear systems via T-S fuzzy modeling. IEEE Trans. on Fuzzy Systems, 2016, 24 (1): 235- 241.
20	HUANG Y, SUN C, QIAN C, et al. Linear parameter varying switching attitude control for a near space hypersonic vehicle with parametric uncertainties. International Journal of Systems Science, 2015, 46 (16): 3019- 3031. doi: 10.1080/00207721.2014.886743
21	HUANG Y, SUN C, QIAN C. Linear parameter varying switching attitude tracking control for a near space hypersonic vehicle via multiple Lyapunov functions. Asian Journal of Control, 2015, 17 (2): 523- 534.
22	WANG Y, JIANG C, WU Q. Attitude tracking control for variable structure near space vehicles based on switched nonlinear systems. Chinese Journal of Aeronautics, 2013, 26 (1): 186- 193.
23	ZHANG Y, JIANG Z, YANG H, et al. High-order extended state observer-enhanced control for a hypersonic flight vehicle with parameter uncertainty and external disturbance. Proc. of the Institution of Mechanical Engineers, Part G:Journal of Aerospace Engineering, 2015, 229 (13): 2481- 2496. doi: 10.1177/0954410015578480
24	CASTAÑEDA H, SALAS-PEÑA O S, DELEÓN-MORALES J. Extended observer based on adaptive second order sliding mode control for a fixed wing UAV. ISA Transactions, 2017, 66, 226- 232. doi: 10.1016/j.isatra.2016.09.013
25	MA D, XIA Y, LI T, et al. Active disturbance rejection and predictive control strategy for a quadrotor helicopter. IET Control Theory & Applications, 2016, 10 (17): 2213- 2222.
26	GUO B Z, ZHAO Z. On the convergence of an extended state observer for nonlinear systems with uncertainty. Systems & Control Letters, 2011, 60 (6): 420- 430.
27	ZHAO Z L, GUO B Z. Extended state observer for uncertain lower triangular nonlinear systems. Systems & Control Letters, 2015, 85, 100- 108.
28	RAN M, WANG Q, DONG C. Stabilization of a class of nonlinear systems with actuator saturation via active disturbance rejection control. Automatica, 2016, 63, 302- 310. doi: 10.1016/j.automatica.2015.10.010
29	WEISSHAAR T A. Morphing aircraft systems:historical perspectives and future challenges. Journal of Aircraft, 2013, 50 (2): 337- 353. doi: 10.2514/1.C031456
30	COLGREN R, KESHMIRI S, MIRMIRANI M. Nonlinear ten-degree-of-freedom dynamics model of a generic hypersonic vehicle. Journal of Aircraft, 2009, 46 (3): 800- 813. doi: 10.2514/1.35644
31	CHEN M, YU J. Disturbance observer-based adaptive sliding mode control for near space vehicles. Nonlinear Dynamics, 2015, 82 (4): 1671- 1682.
32	YOU M, ZONG Q, TIAN B, et al. Comprehensive design of uniform robust exact disturbance observer and fixed-time controller for reusable launch vehicles. IET Control Theory & Applications, 2018, 12 (5): 638- 648.
33	SU R, ZONG Q, TIAN B, et al. Comprehensive design of disturbance observer and non-singular terminal sliding mode control for reusable launch vehicles. IET Control Theory & Applications, 2015, 9 (12): 1821- 1830.
34	SHAO X L, WANG H L. Sliding mode based trajectory linearization control for hypersonic reentry vehicle via extended disturbance observer. ISA Transactions, 2014, 53 (6): 1771- 1786. doi: 10.1016/j.isatra.2014.09.021
35	DONG Q, ZONG Q, TIAN B, et al. Adaptive disturbance observer-based finite-time continuous fault-tolerant control for reentry RLV. International Journal of Robust and Nonlinear Control, 2017, 27 (18): 4275- 4295. doi: 10.1002/rnc.3796
36	WANG X, SHIRINZADEH B. Rapid-convergent nonlinear differentiator. Mechanical Systems and Signal Processing, 2012, 28, 414- 431. doi: 10.1016/j.ymssp.2011.09.026
37	VÁZQUEZ C, ARANOVSKIY S, FREIDOVICH L B, et al. Time-varying gain differentiator:a mobile hydraulic system case study. IEEE Trans. on Control Systems Technology, 2016, 24 (5): 1740- 1750. doi: 10.1109/TCST.2015.2512880
38	FILIPPOV A F. Differential equations with discontinuous righthand sides:control systems. New York: Springer, 1988.
39	JIA Z, YU J, MEI Y, et al. Integral backstepping sliding mode control for quadrotor helicopter under external uncertain disturbances. Aerospace Science and Technology, 2017, 68 (1): 299- 307.
40	HARUNA A, MOHAMED Z, EFE M O, et al. Dual boundary conditional integral backstepping control of a twin rotor MIMI system. Journal of the Franklin Institute, 2017, 354 (15): 6831- 6854. doi: 10.1016/j.jfranklin.2017.08.050
41	RASHAD R, ABOUDONIA A, EI-BADAWY A. A novel disturbance observer-based backstepping controller with command filtered compensation for a MIMI system. Journal of the Franklin Institute, 2016, 353 (16): 4039- 4061. doi: 10.1016/j.jfranklin.2016.07.017
42	POLYAKOV A, FRIDMAN L. Stability notions and Lyapunov functions for sliding mode control systems. Journal of the Franklin Institute, 2014, 351 (4): 1831- 1865. doi: 10.1016/j.jfranklin.2014.01.002
43	MANCILLA-AGUILAR J L, GARCIA R A. On converse Lyapunov theorems for ISS and iISS switched nonlinear systems. Systems & Control Letters, 2001, 42 (1): 47- 53.
44	KHALIL H K. Nonlinear systems. Upper Saddle River, New Jersey: Prentice Hall, 2002.
45	LIBERZON D. Switching in systems and control. New York: Springer Verlag, 2003.

Switching disturbance rejection attitude control of near space vehicles with variable structure

RichHTML

PDF (PC)

可视化

摘要/Abstract

引用本文

使用本文

图/表 12

参考文献 45

相关文章 0

编辑推荐

Metrics

本文评价