Integrated Guidance and Control of Missile Using Subspace Stabilization Method

Abstract:

Integrated guidance and control law is developed for high-maneuvering missile in order to minimize the uncertain dynamic couple between guidance loop and control loop. After building up the integrated model of guidance and control through combining guidance equations and autopilot equations, this paper puts forward a type of subspace control law with attack-angle tracking by using subspace stabilization control method. Finally, the simulation results by an example, which designs the integrated controller for a terminal guided missile, are presented to reveal that the integrated system has good dynamic-tracking performance.

• Periodical: Advanced Materials Research (Volumes 490-495)
• Pages: 1161-1165
• DOI: https://doi.org/10.4028/www.scientific.net/AMR.490-495.1161
• Online since: March 2012
• Authors: Rui Sheng Sun, Peng Yun Liu, Jian Ping Shen
• Keywords: Control Law, Integrated Control, Integrated Guidance, Subspace Stabilization Method

References

[1] C. F. Lin, Q. Wang, J. L. Speyer, et al. Integrated Estimation, Guidance and Control System Design Using Game Theoretic Approach[C]/Proc Ameri Contr Conf, Chicago: [ s, n ] , 1992, pp.3220-3224.

[2] J. H. Evers, J. R. Cloutier, C. F. Lin, et al. Application of Integrated Guidance and Control Schemes to a Precision Guided Missile [C] / Proc Ameri Contr Conf, Chicago: [ s, n ] , 1992, pp.3225-3230.

DOI: 10.23919/acc.1992.4792745

[3] Kuang-Yow Lian, Li-Chen Fu, Dung-Ming Chuang, etc. Nonlinear autopilot and guidance for a highly maneuverable missile[C]. American Control Conference, Vol. 2(1994), pp.2293-2297.

DOI: 10.1109/acc.1994.752487

[4] T. W. Hwang, M. J. Tahk. Integrated Back Stepping Design of Missile Guidance and Control with Robust Disturbance Observer[C]/SICE - ICASE International Joint Conference, Bexco, Busan: [s, n], 2006, pp.4911-4915.

DOI: 10.1109/sice.2006.314847

[5] M. Xin, S. N. Balakrishnan, Ernest J. Ohlmeyer. Integrated Guidance and Control of Missiles With θ-D Method [J]. IEEE Transactions on Control Systems Technology, Vol. 14 No. 6 (2006), pp.981-992.

DOI: 10.1109/tcst.2006.876903

[6] Shtessel Yuri B., Shkolnikov Ilya A. . Integrated Guidance and Control of Advanced Interceptors Using Second Order Sliding Modes[C]. Proceeding of the 42nd IEEE: Conference on Decision and Control, Maui, Hawaii USA, December 2003, pp.4587-4592.

DOI: 10.1109/cdc.2003.1272281

[7] Kim Byoung Soo, Calise Anthony J., Sattigeri Ramachandra J. . Adaptive, Integrated Guidance and Control Design for Line-of-Sight based Formation Flight[C]. AIAA Guidance, Navigation, and Control Conference and Exhibit, 21-24 August 2006, Keystone, Colorado, AIAA 2006-6716.

DOI: 10.2514/6.2006-6716

[8] Tournes C., Paschal N., Wilkerson P. Integrated Terminal Guidance and Automatic Pilot Using Subspace-Stabilization[C]. AIAA-2001-4275.

DOI: 10.2514/6.2001-4275