半捷联位标器稳定跟踪与弹体姿态一体化控制

doi:10.7527/S1000-6893.2016.0128

Abstract

Abstract:

The semi-strapdown coordinator is located on the missile body. Because of the existence of the parasitic loop, the control loop for stable tracking of the semi-strapdown coordinator is strongly coupled with the control loop of the missile body attitude. As a result, the stability and tracking performance of the coordinator are severely affected. In order to solve this problem, an integration control method is proposed. Control law is designed based on the backstepping theory. Stability and dynamic performance of the system can be ensured by choosing an appropriate feedback gain. The integrated control system is verified by simulations. Results show that the integration controller, which considers the coupling between the coordinator stable tracking loop and the missile attitude loop, can not only ensure the dynamic performance of the missile attitude control system, but also improve the stable tracking performance of the coordinator and prevent the high-speed target from escaping from the field of view of the missile seeker.

Key words: semi-strapdown coordinator, stable tracking, attitude control, integration control, backstepping control

CLC Number:

V448.133

YI Ke, CHEN Jian, LIANG Zixuan, REN Zhang, LI Qingdong. Integration control of semi-strapdown coordinator stable tracking and missile body attitude[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2016, 37(12): 3752-3763.

References

[1] 李保平. 战术导弹导引头技术[J]. 弹箭与制导学报, 2002, 22(1):1-5. LI B P. Seeker technique of tactical missile[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2002, 22(1):1-5(in Chinese).
[2] 周瑞青. 捷联导引头稳定与跟踪技术[M]. 北京:国防工业出版社, 2010:1-9. ZHOU R Q. Stabilization and tracking technique for strapdown platform[M]. Beijing:National Defense Industry Press, 2010:1-9(in Chinese).
[3] LIN C L, HSIAO Y H. Adaptive feedforward control for disturbance torque rejection in seeker stabilizing loop[J]. IEEE Transactions on Control Systems Technology, 2001, 9(1):108-121.
[4] 朱华征, 范大鹏, 马东玺, 等. 导引头伺服系统隔离度与测试[J]. 光学精密工程, 2009, 17(8):1993-1998. ZHU H Z, FAN D P, MA D X, et al. Disturbance isolation index of seeker servo system and its test[J]. Optics and Precision Engineering, 2009, 17(8):1993-1998(in Chinese).
[5] 吴晔, 朱晓峰, 陈峻山. 导引头二轴稳定平台的轴角关系和简化[J]. 制导与引信, 2012, 33(1):1-5. WU Y, ZHU X F, CHEN J S. Axis-angle relationships and their simplifications in two-axis stabilied platform of radar seeker[J]. Guidance & Fuze, 2012, 33(1):1-5(in Chinese).
[6] RUDIN R T. Strapdown stabilization for imaging seekers[C]//Proceedings of the 2nd Annual AIAA SDIO Interceptor Technology Conference. Reston:AIAA, 1993:1-10.
[7] 任淼, 王秀萍. 2011年国外空空导弹发展综述[J]. 航空兵器, 2012(3):3-7. REN M, WANG X P. Overview on foreign air-to-air missiles development in 2011[J]. Aero Weaponry, 2012(3):3-7(in Chinese).
[8] 穆学桢, 周树平, 赵桂瑾. AIM-9X空空导弹位标器新技术分析和评价[J]. 红外与激光工程, 2006, 35(4):392-394. MU X Z, ZHOU S P, ZHAO G J.Analysis and evalution of new approach of AIM-9X AAM seeker[J]. Infrared and Laser Engineering, 2006, 35(4):392-394(in Chinese).
[9] 樊会涛. 第五代空空导弹的特点及关键技术[J]. 航空科学技术, 2011(3):1-5. FAN H T. Characteristics and key technologies of the fifth generation of air to air missiles[J]. Aeronautical Science & Technology, 2011(3):1-5(in Chinese).
[10] 赵超. 导引头稳定系统隔离度研究[J]. 电光与控制, 2008, 15(7):78-82. ZHAO C. Study on disturbance rejection rate of a seeker servo system[J]. Electronics Optics &Control, 2008, 15(7):78-82(in Chinese).
[11] 李富贵, 夏群利, 崔晓曦, 等. 导引头隔离度寄生回路对视线角速度提取的影响[J]. 宇航学报, 2013, 34(8):1072-1077. LI F G, XIA Q L, CUI X X, et al. Effect of seeker disturbance rejection rate parasitic loop on line of sight rate extraction[J]. Journal of Astronautics, 2013, 34(8):1072-1077(in Chinese).
[12] 杜运理, 夏群利, 祁载康. 导引头隔离度相位滞后对寄生回路稳定性影响研究[J]. 兵工学报, 2011, 32(1):28-32. DU Y L, XIA Q L, QI Z K. Research on effect of seeker disturbance rejection rate with phase lag on stability of parasitical loop[J]. Acta Armamentarii, 2011, 32(1):28-32(in Chinese).
[13] 李富贵, 夏群利, 祁载康. 导引头隔离度寄生回路对最优制导律性能的影响[J]. 航空学报, 2013, 34(12):2658-2667. LI F G, XIA Q L, QI Z K. Effect of seeker disturbance rejection rate parasitic loop on performance of optimal guidance law[J]. Acta Aeronautica et Astronautica Sinica, 2013, 34(12):2658-2667(in Chinese).
[14] 徐平, 王伟, 林德福. 导引头隔离度对末制导炮弹制导控制的影响[J]. 弹道学报, 2012, 24(1):17-21. XU P, WANG W, LIN D F. Effect of seeker isolation on guidance and control of terminal guided projectile[J]. Journal of Ballistics, 2012, 24(1):17-21(in Chinese).
[15] 姚郁, 章国江. 捷联成像制导系统的若干问题探讨[J]. 红外与激光工程, 2006, 35(1):1-6. YAO Y, ZHANG G J. Discussion on strapdown imaging guidance system[J]. Infrared and Laser Engineering, 2006, 35(1):1-6(in Chinese).
[16] 王志伟, 祁载康, 王江. 滚-仰式导引头跟踪原理[J]. 红外与激光工程, 2008, 37(2):274-277. WANG Z W, QI Z K, WANG J. Tracking principle for roll-pitch seeker[J]. Infrared and Laser Engineering, 2008, 37(2):274-277(in Chinese).
[17] 赵超. 基于角速度补偿的捷联天线稳定系统设计[J]. 电光与控制, 2010, 17(9):60-64. ZHAO C. Design of an angular-rate compensation based strapdown antenna stabilization system[J]. Electronics Optics & Control, 2010, 17(9):60-64(in Chinese).
[18] KENNEDY P J, KENNEDY R L. Direct versus indirect line of sight (LOS) stabilization[J]. IEEE Transactions on Control Systems Technology, 2003, 11(1):3-15.
[19] 周瑞青, 吕善伟, 刘新华. 弹载捷联式天线平台两种稳定实现方法的比较[J]. 系统工程与电子技术, 2005, 27(8):1397-1400. ZHOU R Q, LYU S W, LIU X H. Comparison of two stabilization methods for airborne strapdown antenna platform[J]. Systems Engineering and Electronics, 2005, 27(8):1397-1400(in Chinese).
[20] LIAN B, BANG H, HURTADO J E. Adaptive backstepping control based autopilot design for reentry vehicle[C]//Proceedings of AIAA Guidance, Navigation, and Control Conference and Exhibit. Reston:AIAA, 2004:1-10.
[21] 李菁菁, 任章, 宋剑爽. 高超声速再入滑翔飞行器的模糊变结构控制[J]. 上海交通大学学报, 2011, 45(2):295-300. LI J J, REN Z, SONG J S. Fuzzy sliding mode control for hypersonic re-entry vehicles[J]. Journal of Shanghai Jiaotong University, 2011, 45(2):295-300(in Chinese).

Integration control of semi-strapdown coordinator stable tracking and missile body attitude

PDF (PC)

Knowledge

Abstract

Cite this article

share this article

References

Related Articles 15

Recommended Articles

Metrics

Comments

[1]	Yuqing QIU, Yan LI, Jinxi LANG, Yuxian LIU, Zhong WANG. Robust adaptive attitude control of high-speed helicopters in transition mode [J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(9): 529927-529927.
[2]	Hongyan ZHANG, Wei WANG, Shiwei CHEN, Yi JI, Jiaqi LIU. Integrated guidance and control design based on fully actuated system method [J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(1): 628891-628891.
[3]	Guangquan DUAN, Guoping LIU. Adaptive prescribed control of position and attitude of combined spacecraft based on fully actuated system approach [J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(1): 628837-628837.
[4]	Bing XIAO, Haichao ZHANG. Reinforcement learning robust optimal control for spacecraft attitude stabilization [J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(1): 628890-628890.
[5]	Chao DUAN, Xiaodong SHAO, Qinglei HU, Huaining WU. Attitude tracking of underactuated spacecraft based on transverse function [J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(1): 628910-628910.
[6]	Wu LIU, Yunyan WU, Wei LIU, Mingming TIAN, Tianpeng HUANG. Re-entry robust fault tolerant attitude control for RLVs considering unknown disturbances [J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(S1): 727787-727787.
[7]	Chenyang LIU, Dawei WU, Yize GUO, Xinsai LV, Jiani ZHOU, Shuyi SHAO. Robust adaptive attitude control of quadrotor with uncertain strong coupling [J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(S1): 727645-727645.
[8]	Linkun HE, Wenchao XUE, Ran ZHANG, Huifeng LI. Guidance and control for powered descent and landing of launch vehicles: Overview and outlook [J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(23): 628462-628462.
[9]	Hao ZHANG, Peng WANG, Guojian TANG, Weimin BAO. Event-triggered fast finite time control for hypersonic morphing vehicles [J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(15): 528494-528494.
[10]	Chuang XU, Baolin WU. Distributed fixed-time output-feedback attitude consensus control for multiple spacecraft with input saturation [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(10): 327465-327465.
[11]	WANG Rui, ZHOU Zhou, GUO Ronghua, HUANG Yuechen. Multi-body dynamics simulation and experiment of solar-powered UAV parachute landing [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(8): 225721-225721.
[12]	HU Qinglei, SHAO Xiaodong, YANG Haoyang, DUAN Chao. Spacecraft attitude planning and control under multiple constraints: Review and prospects [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(10): 527351-527351.
[13]	RAN Maopeng, WANG Chengcai, LIU Huahua, WANG Wei, LYU Jinhu. Research status and future development of morphing aircraft control technology [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(10): 527449-527449.
[14]	LIANG Xiaohui, HU Changhua, ZHOU Zhijie, WANG Qing. ADP-based intelligent attitude fault-tolerant control for launch vehicles [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(4): 524915-524915.
[15]	HUANG Xuxing, LI Shuang, YANG Bin, SUN Pan, LIU Xuewen, LIU Xinyan. Spacecraft guidance and control based on artificial intelligence: Review [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(4): 524201-524201.