Entry Trajectory Tracking of RLV Based on Fuzzy Variable Structure Control

doi:10.3969/j.issn.1000-1093.2015.10.011

Abstract

Abstract: To reduce the dependence of trajectory tracking of reusable launch vehicle (RLV) on the aerodynamic parameters and initial conditions, and improve the robustness of traditional control method, a new entry trajectory tracking method based on the fuzzy variable structure is proposed from the perspective of longitudinal tracking guidance. Also, a method of on-line planning the point of the bank angle reversal is designed in the aspect of lateral trajectory control. The simulation results show that the longitudinal tracking control method which is based on the fuzzy variable structure can track the designed trajectory perfectly and stably, and has strong robustness in the condition of big initial state error and aerodynamic coefficient error. The online searching of the bank angle reversal point can be realized by using the proposed lateral guidance method, which can also improve the lateral guidance accuracy effectively.

Key words: control science and technology, reusable launch vehicle, variable structure control, optimization method, fuzzy control, secant method

CLC Number:

V448.235

HU Yu，WANG Hua, REN Zhang. Entry Trajectory Tracking of RLV Based on Fuzzy Variable Structure Control[J]. Acta Armamentarii, 2015, 36(10): 1899-1906.

References

［1］尹佳杰，都延丽，陆宇平.近空间飞行器滑翔再入控制的研究方法与进展[J].飞行力学,2013,31(6):203-208.
YIN Jia-jie, DU Yan-li, LU Yu-ping. Research methods and development of gliding reentry control for near space vehicles[J]. Flight Dynamics, 2013,31(6):203-208. (in Chinese)
[2] Dukeman G A. Profile-following entry guidance using linearquadratic regulatory theory[C]∥AIAA Guidance, Navigation,and Control Conference and Exhibit. Monterey, California：AIAA，2002.
[3] Zhou W Y, Tan S J, Chen H B. A simple reentry trajectory generation and tracking scheme for common aero vehicle[C]∥AIAA Guidance, Navigation,and Control Conference and Exhibit. Minneapolis：AIAA，2012.
[4] 胡跃明.非线性控制系统理论与应用[M].北京：国防工业出版社, 2005:154-175.
HU Yue-ming. Theory and application of nonlinear control system[M]. Beijing：National Defense Industry Press, 2005:154-175. (in Chinese)
[5] 张大元，雷虎民，吴玲，等.基于滑模变结构的弹道跟踪制导律设计[J].系统工程与电子技术, 2014,36(4):721-727.
ZHANG Da-yuan, LEI Hu-min, WU Ling,et al. A trajectory tracking guidance law based on sliding mode variable structure control[J]. Systems Engineering and Electronics. 2014,36 (4):721-727.(in Chinese)
[6] Shen Z J. On-board three-dimensional constrained entry flight trajectory generation[J]. Dissertation Abstracts International, 2002, 63(8):3804.
[7] Yousef H, A, Hamdy M, Shafiq M. Adaptive fuzzy-based tracking control for a class of strict-feedback SISO nonlinear time-delay systems without backstepping[J]. International Journal of Unicertainty, Fuzziness and Knowledge-Based System, 2012, 20(3): 339- 353.
[8] 胡剑波. 一类非匹配不确定性系统的变结构控制[J]. 控制理论与应用, 2002, 19(1):105-108.
HU Jian-bo. Variable structure control for a class of systems with mismatched uncertainties[J]. Control Theory and Application, 2002,19(1):105-108. (in Chinese)
[9] 周凤岐，王延，周军，等. 高超声速飞行器耦合系统变结构控制设计[J]. 宇航学报, 2011, 32(1):66-71.
ZHOU Feng-qi, WANG Yan, ZHOU Jun,et al. Design of variable structure controller for hypersonic coupled vehicle system[J]. Journal of Astronautics, 2011, 32(1):66-71.(in Chinese)
[10] Ha Quang Thinh Ngo, Jin-Ho Shin, Won-Ho Kim. Fuzzy sliding mode control for a robot manipulator[J]. Artificial Life and Robotics. 2008,13(1):124-128.
[11] Ping L. An alternative entry guidance scheme for the X-33[J]. American Institute of Aeronautics and Astronautics. 1998(8):189-199.
[12] 赵汉元.航天器再入制导方法综述[J]. 航天控制, 1994(1):345-348.
ZHAO Han-yuan. A survey of guidance methods for spacecraft reentry[J]. Aerospace Control, 1994(1):345-348. (in Chinese)

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