高超声速飞行器纵向大攻角非线性失稳分析与控制

doi:10.7527/S1000-6893.2016.0172

Abstract

Abstract:

Bifurcation and continuation method is employed to address the issue of longitudinal loss of stability of high angle of attack of hypersonic glide vehicle. Based on the obtained codimension 1 equilibrium bifurcation branches presented in phase-parameter space, the stability of the branches and catastrophe are analyzed. The codimension 2 equilibrium bifurcation branches are then presented in phase-parameter space. The 3D surface of equilibrium for the full Mach number and angle of attack parameter space are given, including stable and unstable branch surfaces. The nonlinear dynamic inversion is utilized to design the controller for longitudinal dynamics. The overall open-loop and closed-loop eigenvalue are plotted. A new evaluation strategy for nonlinear closed-loop dynamics is proposed to evaluate the overall performance of the designed controller. Time-history simulation is combined to verify the efficacy and high performance of the controller.

Key words: hypersonic vehicle, longitudinal flight with high angle of attack, bifurcation and catastrophe, nonlinear loss of stability, nonlinear control

CLC Number:

V211

SU Erlong, LUO Jianjun, MIN Changwan. Analysis and control of nonlinear loss of stability for longitudinal flight dynamics of hypersonic vehicle with high angle of attack[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2016, 37(S1): 80-90.

References

[1] 叶友达. 近空间高速飞行器气动特性研究与布局设计优化[J]. 力学进展, 2009, 39(6):683-694. YE Y D. Study on aerodynamics characteristics and design optimization for high speed near space vehicles[J]. Advance in Mechanics, 2009, 39(6):683-694 (in Chinese).
[2] 张鲁民. 航天飞机空气动力学分析[M]. 北京:国防工业出版社, 2009:30-40. ZHANG L M. Analysis of space shuttle aerodynamics[M]. Beijing:National Defense Industry Press, 2009:30-40 (in Chinese).
[3] CARROLL J V, MEHRA R K. Bifurcation analysis of nonlinear aircraft dynamics[J]. Journal of Guidance, Control, and Dynamics, 1982, 5(5):529-536.
[4] GOMAN M G, KHRAMTSOVSKY A V. Application of continuation and bifurcation methods to the design of control systems[J]. Philosophical Transactions of the Royal Society of London, Series A:Mathematical, Physical and Engineering Sciences, 1998, 356 (1745):2277-2295.
[5] PASHILKAR A A, PRADEEP S. Computation of flight mechanics parameters using continuation techniques[J]. Journal of Guidance, Control, and Dynamics, 2001, 24(2):324-329.
[6] AMIT K K, JATINDER S. Aircraft design using constrained bifurcation and continuation method[J]. Journal of Aircraft, 2014, 51(5):1647-1652.
[7] LEE H P, CHANG M, KAISER M K. Flight dynamics and stability and control characteristics of the X-33 technology demonstrator vehicle:AIAA-1998-4410[R]. Reston:AIAA, 1998.
[8] PHILIP C. An entry flight controls analysis for a reusable launch vehicle:AIAA-2000-1046[R]. Reston:AIAA, 2000.
[9] TANCREDI U, GRASSI M, VERDE L, et al. Aerodynamics uncertainties compliance with desired lateral-directional dynamics for an unmanned space vehicle:AIAA-2005-6962[R]. Reston:AIAA, 2005.
[10] 祝立国, 王永丰, 庄逢甘, 等. 高速高机动飞行器的横航向偏离预测判据分析[J]. 宇航学报, 2007, 28 (6):1550-1553. ZHU L G, WANG Y F, ZHUANG F G, et al. The lateral-directional departure criteria analysis of high-speed and high maneuverability aircraft[J]. Journal of Astronautics, 2007, 28(6):1550-1553 (in Chinese).
[11] 祝立国, 王永丰, 庄逢甘, 等. Weissman图的产生、发展及其在再入航天飞行器气动布局设计中的应用[J]. 宇航学报, 2009, 30 (1):13-17. ZHU L G, WANG Y F, ZHUANG F G, et al. The derivation, development of Weissman chart and applications on configuration design of reentry vehicle[J]. Journal of Astronautics, 2009, 30(1):13-17 (in Chinese).
[12] 高清, 赵俊波, 李潜. 类HTV-2横侧向稳定性研究[J]. 宇航学报, 2014, 35(6):657-662. GAO Q, ZHAO J B, LI Q. Study on lateral-directional stability of HTV-2 like configuration[J]. Journal of Astronautics, 2014, 35(6):657-662 (in Chinese).
[13] 高清, 李建华, 李潜. 升力体高超声速飞行器横向气动特性研究[J]. 实验流体力学, 2015, 29(1):43-48. GAO Q, LI J H, LI Q. Study on lateral stability of hypersonic lifting-configurations[J]. Journal of Experiments in Fluid Mechanics, 2015, 29(1):43-48 (in Chinese).
[14] KUZNETSOV Y A. Elements of applied bifurcation theory[M]. 3rd ed. New York:Springer-Verlag, 2004.
[15] STEPHEN J G, MARK H L, SIMON A N. Upset dynamics of an airliner model:A nonlinear bifurcation analysis[J]. Journal of Aircraft, 2013, 50(6):1832-1842.

Analysis and control of nonlinear loss of stability for longitudinal flight dynamics of hypersonic vehicle with high angle of attack

PDF (PC)

Knowledge

Abstract

Cite this article

share this article

References

Related Articles 15

Recommended Articles

Metrics

Comments

[1]	Bo YANG, He YU, Zichen FAN. Micro-energy analysis method for time-varying error of aero-optical effects [J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(4): 128703-128703.
[2]	Weilin NI, Yonghai WANG, Cong XU, Fenghua CHI, Haizhao LIANG. Cooperative game guidance method for hypersonic vehicles based on reinforcement learning [J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(S2): 729400-729400.
[3]	Ping MA, Ning ZHANG, Anhua SHI, Zhefeng YU, Shichang LIANG, Jie HUANG. Transmission characteristics of typical band microwave in experiment⁃simulated plasma [J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(S2): 729476-729476.
[4]	Ziyi WU, Shaoming HE, Yadong WANG, Hongyan LI. Nonlinear observability-enhancement optimal guidance law for moving targets [J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(S2): 729750-729750.
[5]	Yuemeng MA, Ming LIU, Ding YANG, Ming YANG, Mingang ZHANG, Yajie GE. Prescribed performance and anti⁃noise control of near space vehicle with thermal constraint [J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(S2): 729390-729390.
[6]	Haoyu CHEN, Binwen WANG, Qiaozhi SONG, Xiaodong LI. Thermal flutter ground simulation test [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(8): 227295-227295.
[7]	Ziyi WANG, Weiwei ZHANG, Lei LIU, Xiaofeng YANG. Reduced order aerothermoelastic framework suitable for complex flow [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(4): 126807-126807.
[8]	Xunliang YAN, Peichen WANG, Shumei WANG, Yuxuan YANG, Kuan WANG. Rapid robust trajectory optimization for RBCC vehicle ascent based on polynomial chaos [J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(21): 528349-528349.
[9]	Zhikun SUN, Zhiwei SHI, Weilin ZHANG, Zheng LI, Qijie SUN. Effect of plasma actuator on lift-drag characteristics of high-speed airfoil [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(S2): 23-39.
[10]	ZHENG Hui, QIU Lei, YUAN Shenfang, YANG Xiaofei, LU Xulong, XUE Zhaopeng. Experimental method of guided wave monitoring for high temperature airflow damage of C/C thermal protection structures [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(8): 225659-225659.
[11]	SUN Cong. Development status, challenges and trends of strength technology for hypersonic vehicles [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(6): 527590-527590.
[12]	LUO Shibin, MIAO Zhichao, SONG Jiawen. Influencing factors of active cooling at leading edge of hypersonic vehicles [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(12): 627023-627023.
[13]	GAO Chang, LI Zhengzhou, HUANG Jiangtao, HE Yuanyuan, WU Yingchuan, LE Jialing, GUI Feng. High-accuracy aerodynamic optimization of hypersonic vehicles based on continuous adjoint [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(7): 124490-124490.
[14]	WEI Kepeng, HU Jian, YAO Jianyong, XING Haochen, LE Guigao. Fast terminal sliding mode control of neural networks for aeromechanical actuators [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(6): 624540-624540.
[15]	HE Wei, FANG Yongchun, LIANG Xiao, ZHANG Peng. Design and implementation of a 2-DOF aerial manipulation system [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(2): 324280-324280.