Research of Trajectory Tracking Control of Cruise Missile Based on Observer

Abstract:

To achieve cruise missile accurate trajectory tracking control, an observer-based tracking control method is designed. An observer is developed to estimate the states and control signals of desired trajectory as the inputs of the tracking controller. The linear quadratic optimal control is used to realize full-state feedback control for trajectory tracking. A certain cruise missile is used for the tracking simulation and the result shows satisfactory performance, the control method is simple and suitable for engineering applications.

• Periodical: Applied Mechanics and Materials (Volumes 184-185)
• Pages: 1599-1602
• DOI: https://doi.org/10.4028/www.scientific.net/AMM.184-185.1599
• Online since: June 2012
• Authors: Bo Hao, Fan Li, Jian Hui Zhao
• Keywords: Cruise Missile, Observer, Quadratic Optimal Control, Trajectory Tracking

References

[1] Yagimli, M.Simsir, U.Tozan, H." Trajectory tracking of a satellite communicated missile with Fuzzy and PID control," Recent Advances in Space Technologies (RAST), 2011 5th International Conference on 2011, pp: 318 -323.

DOI: 10.1109/rast.2011.5966848

[2] Tsai, Ching-Chih . Ju, Shiang-Yun. "Trajectory tracking and regulation of a self-balancing two-wheeled robot : A backstepping sliding-mode control approach , " Proceedings of the SICE Annual Conference,2010,pp:  2411-2418 .

DOI: 10.1109/iros.2010.5652351

[3] Tsai, CC, Lee, CT ,Hwang, KS."Intelligent Adaptive Trajectory Tracking Control Using Fuzzy Basis Function Networks for an Autonomous Small-Scale Helicopter," 2011 IEEE International Conference on Systems, Man, and Cybernetics(SMC),2011: 2249-2254 .

DOI: 10.1109/icsmc.2011.6084012

[4] Xie Zhufeng, Xia Yuanqing, Fu Mengyin. " Robust trajectory-tracking method for UAV using nonlinear dynamic inversion," Proceedings of the 2011 IEEE 5th International Conference on Cybernetics and Intelligent Systems, 2011,pp: 93-98 .

DOI: 10.1109/iccis.2011.6070308

[5] Kim, B.-M, Kim, B.S, Kim, N.-W. " Trajectory tracking controller design using neural networks for a tiltrotor unmanned aerial vehicle," Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering,  VOL 224,2010,pp: 881-896 .

DOI: 10.1243/09544100jaero710

[6] Song C H, Kim S J, Kim S H, et al. "Robust Control of The Missile Attitude Based on Quaternion Feedback,"Control Engineering Practice, 2006, 14(3),pp:811-818.

DOI: 10.1016/j.conengprac.2005.04.003

[7] Xu Yang, Xin Yi. "LQR-based Design and Research for Trajectory Control System of Guided Bomb Unit ,"Tactical Missile Technology, 2010, 5,pp:84-87.

[8] Minghao Wang ,Gang Liu ,Hongqing Hou. "Design of BTT Control Technology for Cruise Missile Based on LQR,"2011 2nd International Conference on Artificial Intelligence, Management Science and Electronic Commerce, 2011,pp: 3875-3878 .

DOI: 10.1109/aimsec.2011.6009996