弹性高超声速飞行器动态面制导控制一体化设计方法

doi:10.12305/j.issn.1001-506X.2022.03.28

Abstract

Abstract:

Two integrated guidance and control methods based on dynamic surface control theory are designed for flexible hypersonic vehicles in glide phase. The longitude translational and rotational equations of flexible hypersonic vehicles in glide phase are denoted. A strict-feedback integrated guidance and control design model for flexible hypersonic vehicles is deduced. The flexible states of the hypersonic vehicle are regarded as uncertainties. Two integrated guidance and control schemes are proposed based on adaptive approach and nonlinear disturbance observer (NDO) technique, respectively. The states of the closed-loop systems are proved to be uniformly ultimately bounded based on Lyapunov stability theorem. Simulation experiments are conducted to verify the effectiveness and robustness of the proposed schemes. The performance differences between the two schemes and the reasons behind are analyzed further.

Key words: flexible hypersonic vehicle, dynamic surface control method, integrated guidance and control, adaptive approach, nonlinear disturbance observer (NDO)

CLC Number:

V448

Tong AN, Peng WANG, Jianhua WANG, Guojian TANG, Yulong PAN, Haishan CHEN. Integrated guidance and control schemes for dynamic surface of flexible hypersonic vehicles[J]. Systems Engineering and Electronics, 2022, 44(3): 956-966.

Figures/Tables 11

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References 30

1	XU B , SHI Z A . An overview on flight dynamics and control approaches for hypersonic vehicles[J]. Science China Information Sciences, 2015, 58 (7): 819- 838.
2	程仙垒. 弹性高超声速飞行器鲁棒自适应控制方法研究[D]. 长沙: 国防科技大学, 2018.
	CHENG X L. Robust adaptive control for flexible hypersonic vehicles[D]. Changsha: National University of Defense Techno-logy, 2018.
3	ZHAO T H , WANG P , LIU L P , et al. Integrated guidance and control with L2 disturbance attenuation for hypersonic vehicles[J]. Advances in Space Research, 2016, 57 (12): 2519- 2528. doi: 10.1016/j.asr.2016.03.042
4	王建华, 刘鲁华, 王鹏, 等. 高超声速飞行器俯冲段制导控制一体化设计方法[J]. 航空学报, 2017, 38 (3): 202- 214.
	WANG J H , LIU L H , WANG P , et al. Integrated guidance and control for hypersonic vehicles in dive phase[J]. Acta Aeronautica et Astronautica Sinica, 2017, 38 (3): 202- 214.
5	严晗. 鲁棒非线性导引与控制律一体化设计研究[D]. 合肥: 中国科学技术大学, 2013.
	YAN H. Research on robust nonlinear integrated guidance and control design[D]. Hefei: University of Science and Technology of China, 2013.
6	ZHOU H T , ZHAO H , HUANG H F , et al. Integrated guidance and control design of the suicide UCAV for terminal attack[J]. Journal of System Engineering and Electronics, 2017, 28 (3): 546- 555. doi: 10.21629/JSEE.2017.03.14
7	LIU X H , HUANG W F , DU L . An integrated guidance and control approach in three-dimensional space for hypersonic missile constrained by impact angles[J]. ISA Trans, 2017, 66, 164- 175. doi: 10.1016/j.isatra.2016.10.008
8	WANG W P , XIONG S S , WANG S T , et al. Three dimensional impact angle constrained integrated guidance and control for missiles with input saturation and actuator failure[J]. Aerospace Science and Technology, 2016, 53, 169- 187. doi: 10.1016/j.ast.2016.03.015
9	HOU M , DUAN G S . Adaptive dynamic surface control for integrated missile guidance and autopilot[J]. International Journal of Automation and Computing, 2011, 8 (1): 122- 127. doi: 10.1007/s11633-010-0563-z
10	AI X L , SHEN Y C , WANG L L . Adaptive integrated guidance and control for impact angle constrained interception with actuator saturation[J]. The Aeronautical Journal, 2019, 123 (1267): 1437- 1453. doi: 10.1017/aer.2019.71
11	王鹏, 鲍存余, 汤国建. 高超声速飞行器滑翔段制导姿控一体化设计方法研究[J]. 战术导弹技术, 2020, (5): 127- 138.
	WANG P , BAO C Y , TANG G J . Research on design of integrated guidance and attitude control for hypersonic vehicle in glide phase[J]. Tactical Missile Technology, 2020, (5): 127- 138.
12	ZHOU X D , WANG W H , LIU Z , et al. Impact angle constrained three-dimensional integrated guidance and control based on fractional integral terminal sliding mode control[J]. IEEE Access, 2019, 7, 126857- 126870. doi: 10.1109/ACCESS.2019.2939418
13	MING C M , WANG X F , SUN R Z . A novel non-singular terminal sliding mode control-based integrated missile guidance and control with impact angle constraint[J]. Aerospace Science and Technology, 2019, 94, 105368. doi: 10.1016/j.ast.2019.105368
14	JIANG S T , TIAN F H , SUN S . Integrated guidance and control design of rolling-guided projectile based on adaptive fuzzy control with multiple constraints[J]. Mathematical Problems in Engineering, 2019, 2019, 324- 337.
15	赖超, 王卫红, 周本春, 等. 三维攻击角度约束部分制导控制一体化设计[J]. 宇航学报, 2019, 40 (8): 937- 947.
	LAI C , WANG W H , ZHOU B C , et al. Three-dimensional partial integrated guidance and control with impact angle constraints[J]. Journal of Astronautics, 2019, 40 (8): 937- 947.
16	LI G S , CHAO T , WANG S , et al. Integrated guidance and control for the fixed-trim vehicle against the maneuvering target[J]. International Journal of Control, Automation and Systems, 2020, 18 (6): 1518- 1529. doi: 10.1007/s12555-018-0824-0
17	JIANG S , TIAN F Q , SUN S Y , et al. Integrated guidance and control of guided projectile with multiple constraints based on fuzzy adaptive and dynamic surface[J]. Defence Technology, 2020, 16 (6): 1130- 1141. doi: 10.1016/j.dt.2019.12.003
18	SONG H T , ZHANG T . Fast integrated guidance and control with global convergence[J]. Journal of Central South University, 2019, 26 (3): 632- 639. doi: 10.1007/s11771-019-4034-6
19	毛柏源, 李君龙, 张锐, 等. 大姿控力矩复合控制导弹制导控制一体化设计[J]. 现代防御技术, 2019, 47 (3): 56- 63. doi: 10.3969/j.issn.1009-086x.2019.03.09
	MAO B Y , LI J L , ZHANG R , et al. Integrated guidance and control for blended control missile using large attitude control moment[J]. Modern Defense Technology, 2019, 47 (3): 56- 63. doi: 10.3969/j.issn.1009-086x.2019.03.09
20	WANG P M , ZHANG X , ZHU J T . Integrated missile guidance and control: a novel explicit reference governor using a disturbance observer[J]. IEEE Trans.on Industrial Electro-nics, 2019, 66 (7): 5487- 5496. doi: 10.1109/TIE.2018.2868300
21	BOLENDER M, DOMAN D. A non-linear model for the longitudinal dynamics of a hypersonic air-breathing vehicle[C]//Proc. of the AIAA Guidance, Navigation, and Control Confe-rence and Exhibit, 2005.
22	BOLENDER M A , DOMAN D B . Nonlinear longitudinal dynamical model of an air-breathing hypersonic vehicle[J]. Journal of Spacecraft and Rockets, 2007, 44 (2): 374- 387. doi: 10.2514/1.23370
23	SIGTHORSSON D O , JANKOVSKY P , SERRANI A , et al. Robust linear output feedback control of an airbreathing hypersonic vehicle[J]. Journal of Guidance, Control, and Dynamics, 2008, 31 (4): 1052- 1066. doi: 10.2514/1.32300
24	SIGTHORSSON D, SERRANI A. Development of linear parameter-varying models of hypersonic air-breathing vehicles[C]// Proc. of the AIAA Guidance, Navigation, and Control Confe-rence, 2009.
25	FIORENTINI L. Nonlinear adaptive controller design for air-breathing hypersonic vehicles[D]. Columbus: The Ohio State University, 2010.
26	ZONG Q , WANG F , TIAN B S , et al. Robust adaptive approximate backstepping control of a flexible air-breathing hypersonic vehicle with input constraint and uncertainty[J]. Proceedings of the Institution of Mechanical Engineers, Part Ⅰ: Journal of Systems and Control Engineering, 2014, 228 (7): 521- 539.
27	ZONG Q P , WANG F S , SU R , et al. Robust adaptive backstepping tracking control for a flexible air-breathing hypersonic vehicle subject to input constraint[J]. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2014, 229 (1): 10- 25.
28	BU X , WU X , HUANG J , et al. Minimal-learning-parameter based simplified adaptive neural back-stepping control of flexible air-breathing hypersonic vehicles without virtual controllers[J]. Neurocomputing, 2016, 175, 816- 825.
29	YE L , ZONG Q , TIAN B , et al. Control-oriented modeling and adaptive backstepping control for a nonminimum phase hypersonic vehicle[J]. ISA Trans, 2017, 70, 161- 172.
30	王建华, 刘鲁华, 王鹏, 等. 高超声速飞行器纵向平面滑翔飞行制导控制方法[J]. 国防科技大学学报, 2017, 39 (1): 58- 66.
	WANG J H , LIU L H , WANG P , et al. Longitudinal integrated guidance and control scheme for hypersonic vehicle in glide phase[J]. Journal of National University of Defense Technology, 2017, 39 (1): 58- 66.

IGC方法	设计参数
自适应	k₁=k₂=2 k₃=8	τ₂=τ₃=0.5	ε₁=ε₂=ε₃=10 σ₁=σ₂=σ₃=1
NDO	${\bar k}$₁=${\bar k}$₂=2 ${\bar k}$₃=8	τ₂=τ₃=0.5	l₁=0.7 l₂=l₃=0.5

编号	参数偏差组合	标识线型	脱靶量/m
编号	参数偏差组合	标识线型	自适应	NDO
①	ρ+30% C_L、C_D+20%, m_z+20%	红色实线	0.52	1.00
②	ρ+30% C_L、C_D+20%, m_z-20%	绿色虚线	1.73	0.53
③	ρ+30%, C_L、C_D-20%, m_z-20%	蓝色点线	1.76	3.21
④	ρ+30%, C_L、C_D-20%, m_z+20%	橙色短点线	2.53	2.61
⑤	ρ-30% C_L、C_D+20% m_z+20%	□形红色实线	1.66	8.66
⑥	ρ-30%, C_L、C_D+20%, m_z-20%	○形绿色虚线	0.96	12.72
⑦	ρ-30%, C_L、C_D-20%, m_z-20%	△形蓝色点线	12 449.77	39.32
⑧	ρ-30%, C_L、C_D-20% m_z+20%	◇形橙色短点线	12 430.97	34.72

[1]	Shang JIANG, Bo WEI, Weige LIANG, Dongyan SUN, Jinjun LI, Ye MA. Integrated guidance and control design method with multiple constraints and backlash [J]. Systems Engineering and Electronics, 2022, 44(4): 1318-1328.
[2]	TAO Fuyu, WANG Tong, XIA Yueming. Angle Doppler compensation method and improvement approaches of non sidelooking array based on IAA [J]. Systems Engineering and Electronics, 2019, 41(2): 291-297.
[3]	ZHAO Kun, CAO Dengqing, HUANG Wenhu. Integrated design of maneuver, guidance and control for penetration missile [J]. Systems Engineering and Electronics, 2018, 40(9): 2040-2047.
[4]	XIA Chuan, DONG Chaoyang, WANG Qing, CHENG Haoyu. Adaptive integrated guidance and control backstepping sliding mode design for blended control missile#br# [J]. Systems Engineering and Electronics, 2018, 40(10): 2325-2333.
[5]	LU Xiaodong, ZHAO Hui, ZHAO Bin, ZHOU Jun. Novel backstepping attitude control method for interception missile based on disturbance compensation [J]. Systems Engineering and Electronics, 2017, 39(5): 1100-1106.
[6]	QI Hui1, ZHANG Ze1, HAN Pengxin2, XU Jiangtao1, ZHANG Dewei1. Integrated design of missile guidance and control based onbackstepping and sliding mode control [J]. Systems Engineering and Electronics, 2016, 38(3): 618-623.
[7]	DONG Chao-yang, CHENG Hao-yu, WANG Qing. Backstepping sliding mode control for integrated guidance and#br# control design based on active disturbance rejection [J]. Systems Engineering and Electronics, 2015, 37(7): 1604-1610.
[8]	WANG Xiao-fang， ZHENG Yi-yu， LIN Hai. 4D integrated guidance and control law for missiles cooperative engagement [J]. Systems Engineering and Electronics, 2015, 37(4): 874-881.
[9]	SU Lei, YAO Hong, DU Jun. NDO based antidisturbance control law design for#br# aircraft trajectory tracking [J]. Systems Engineering and Electronics, 2014, 36(9): 1804-1809.
[10]	WEN Cai, WANG Tong, WU Jian-xin. Direct data domain approach with iterative space-time adaptive processing [J]. Systems Engineering and Electronics, 2014, 36(5): 831-837.
[11]	SU Lei, YAO Hong, DU Jun, YANG Jun-feng. Adaptive backstepping terminal sliding mode control for aircraft trajectory tracking [J]. Systems Engineering and Electronics, 2014, 36(11): 2249-2254.
[12]	YIN Yong-xin1，SHI Wen1，YANG Ming2. Integrated guidance and control based on dynamic inverse and extended state observer method [J]. Journal of Systems Engineering and Electronics, 2011, 33(6): 1342-1345.
[13]	WANG Jian-hao, HU Jian-bo, GAO Peng. Tracking control of flight simulator servo systems based on NDO [J]. Journal of Systems Engineering and Electronics, 2011, 33(10): 2301-2305.

Integrated guidance and control schemes for dynamic surface of flexible hypersonic vehicles

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