升力式再入飞行器大动压下横侧向RCS姿态控制方法研究 -- 西北工业大学学报,2019,37(1):21-27
论文:2019,Vol:37,Issue(1):21-27
引用本文:
樊朋飞, 凡永华, 闫杰. 升力式再入飞行器大动压下横侧向RCS姿态控制方法研究[J]. 西北工业大学学报
FAN Pengfei, FAN Yonghua, YAN Jie. Lateral/Directional RCS Attitude Control for Lift Reentry Vehicle in Large Dynamic Pressure Regime[J]. Northwestern polytechnical university

升力式再入飞行器大动压下横侧向RCS姿态控制方法研究
樊朋飞, 凡永华, 闫杰
西北工业大学 航天学院, 陕西 西安 710072
摘要:
针对升力式再入飞行器大动压下横侧向快速、高精度RCS姿态控制问题,利用再入飞行器在大攻角状态下横侧向耦合明显,偏航通道对倾侧角的控制更高效、抗干扰能力更强的特点,提出了同时控制滚转和偏航跟踪倾侧角指令的策略,设计了以倾侧角控制为外回路,以滚转和偏航角速率为内回路的双回路动态逆控制器。通过滚转角速率控制器的改进设计保证了侧滑角在不受控状态下的收敛性,并分析了控制参数选择对侧滑角收敛特性的影响。将该控制器与采用常规解耦方式设计的控制器进行了仿真对比,结果表明,该方法有效解决了采用常规RCS控制方法时倾侧角在大动压再入条件下响应慢、抗干扰能力差的问题,提高了RCS在大动压下的控制能力。
关键词:    再入飞行器    横侧向控制    反作用控制系统    动态逆   
Lateral/Directional RCS Attitude Control for Lift Reentry Vehicle in Large Dynamic Pressure Regime
FAN Pengfei, FAN Yonghua, YAN Jie
School of Astronautics, Northwestern Polytechnical University, Xi'an 710072, China
Abstract:
For the existence of aerodynamic coupling and big turbulence of reentry vehicle in large aerodynamic flight status, Conventional method for RCS controller designing is difficult to track the bank angle command quickly and accurately. To solve the problem, according to the feature that the lateral/directional coupling is significant and the yaw channel is more effective and stronger to turbulence when tracking the bank angle, a strategy is proposed by using the roll and yaw channel simultaneously to control the bank angle dynamic. Double loop dynamic inversion controller is designed in which the bank angle loop conduct as outer loop and the roll and yaw angle rate loop as inner loop. The convergence of sideslip angle is guaranteed by improving the design of roll angle rate controller and the influence of the controller parameters to converge mode is analyzed. PWPF modulator is applied to convert command moment into pulse signals. Numerical simulation is carried out to verify the benefits of the proposed control method, the results shows that the present method solved the problem that RCS controller designed in conventional manner, and improve control ability of RCS in large aerodynamic condition.
Key words:    reentry vehicle    lateral flight control    reaction control system    dynamic inversion   
收稿日期: 2018-03-12     修回日期:
DOI: 10.1051/jnwpu/20193710021
通讯作者:     Email:
作者简介: 樊朋飞(1986-),西北工业大学博士研究生,主要从事飞行器制导控制系统设计研究。
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参考文献:
[1] 房元鹏. 可重复使用航天器反作用力控制系统控制方法[J]. 航空学报,2008,29(增刊1):97-101 FANG Yuanpeng. Reaction Control System Control Method for Reusable Launch Vehicle[J]. Acta Aeronautica et Astronautica Sinica, 2008, 29(suppl 1):97-101 (in Chinese)
[2] 史丽楠,李惠峰,张冉. 滑翔再入飞行器横侧向耦合姿态控制策略[J]. 北京航空航天大学学报,2016,42(1):120-129 SHI Linan, LI Huifeng, ZHANG Ran. Gliding Reentry Vehicle Lateral/Directional Coupling Attitude Control Strategy[J]. Journal of Beijing University of Aeronautics and Astronautics, 2016, 42(1):120-129 (in Chinese)
[3] 郭建国,张添保,周军,等. 再入飞行器的RCS控制系统设计[J]. 固体火箭技术,2017,40(4):511-516 GUO Jianguo, ZHANG Tianbao, ZHOU Jun, et al. Reaction Control System Design for Reentry Vehicle[J]. Journal of Solid Rocket Technology, 2017, 40(4):511-516 (in Chinese)
[4] 贺成龙,陈欣,吴了泥. 可重复使用运载器的RCS姿态控制技术研究[J]. 弹箭与制导学报,2010,30(1):51-54 HE Chenglong, CHEN Xin, WU Liaoni. Research on Attitude Control of Reaction Control System for Reusable Launch Vehicle[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2010, 30(1):51-54 (in Chinese)
[5] MATHAVARAJ S, OMKAR Halbe, RADHAKANT Padhi. Robust Control of a Reusable Launch Vehicle in Reentry Phase Using Model Following Neuro-Adaptive Design[R]. AIAA-2010-8312
[6] 陈海兵,张曙光,方振平. 加速度反馈的隐式动态逆鲁棒非线性控制律设计[J]. 航空学报,2009,30(4):597-603 CHEN Haibing, ZHANG Shuguang, FANG Zhenping. Implicit NDI Robust Nonlinear Control Design with Acceleration Feedback[J]. Acta Aeronautica et Astronautica Sinica, 2009, 30(4):597-603 (in Chinese)
[7] 王霄婷,周军,林鹏. 再入飞行器变质心/RCS复合控制策略研究[J]. 西北工业大学学报,2011,29(2):212-216 WANG Xiaoting, ZHOU Jun, LIN Peng. Proposing Moving Centroid/RCS Control Strategy for Reentry Flight Vehicle[J]. Journal of Northwestern Polytechnical University, 2011, 29(2):212-216 (in Chinese)
[8] 宁国栋,张曙光,方振平. 跨大气层飞行器再入段RCS控制特性[J]. 飞行力学,2005,23(3):16-20 NING Guodong, ZHANG Shuguang, FANG Zhenping. Research on the Reaction Control System for Spacecraft Re-Entry Flight[J]. Flight Dynamics, 2005, 23(3):16-20 (in Chinese)
[9] 陆艳辉,张曙光. 离散RCS的PWPF调制方式改进及混合控制逻辑设计[J]. 航空学报,2012,33(9):1561-1570 LU Yanhui, ZHANG Shuguang. An Improvement on PWPF Modulation of Discrete RCS and Design of the Blended Control Logic[J]. Acta Aeronautica et Astronautica Sinica, 2012, 33(9):1561-1570 (in Chinese)
[10] 吴宏鑫,孟斌. 高超声速飞行器控制研究综述[J]. 力学进展,2009,39(6):756-765 WU Hongxin, MENG Bin. Review on The Control of Hypersonic Flight Vehicles[J]. Advances in Mechanics, 2009, 39(5):756-765 (in Chinese)
[11] 刘军,黄一敏,孙春贞,等. 高超声速飞行器再入段RCS姿态控制[J]. 兵工自动化,2014,33(3):47-50 LIU Jun, HIANG Yimin, SUN Chunzhen, et al. Research on Attitude Control of Reaction Control System for Hypersonic Vehicle[J]. Oranance Industry Automation, 2014, 33(3):47-50 (in Chinese)
[12] KROVEL T D. Optimal Tuning of PWPF Modulator for Attitude Control[D]. Trondheim, Norway, Norway University of Science and Technology, 2005
[13] HE Jingjing, QI Ruiyun, JIANG Bin, et al. Fault-Tolerant Control with Mixed Aerodynamic Surfaces and RCS Jets for Hypersonic Reentry Vehicles[J]. Chinese Journal of Aeronautics, 2017, 30(2):780-795
[14] ELMAR M W, KLAUS H W. Attitude Control of a Reentry Vehicle with Internal Dynamics[R]. AIAA-2002-4647
[15] DACOSTA R R, CHU Q P, MULDER J A. Reentry Flight Controller Design Using Nonlinear Dynamic Inversion[J]. Journal of Spacecraft and Rockets, 2003, 40(1):64-71
[16] MOOIJ E. Adaptive Lateral Flight Control for a Wings Re-Entry Vehicle[R]. AIAA-2003-5322
[17] RAMSES M A. Robust Failure Detection for Reentry Vehicle Attitude Control Systems[J]. Journal of Guidance Control and Dynamic,1999, 22(6):839-845