A New Angular Acceleration Guidance Law with Estimation Approach Based on Sliding Mode Observer against High Maneuvering Target

Yuan Yun Song; Wan Chun Chen; Xing Liang Yin

doi:10.4028/www.scientific.net/AMM.110-116.5249

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HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vols. 110-116A New Angular Acceleration Guidance Law with...

A New Angular Acceleration Guidance Law with Estimation Approach Based on Sliding Mode Observer against High Maneuvering Target

Abstract:

A new type of guidance law is developed for intercepting high maneuvering target. The law takes angular acceleration of line-of-sight as a primary input in place of the acceleration of target. As the significant required input quantity of the angular acceleration guidance (AAG), the angular acceleration of line-of-sight is estimated by a developed estimation approach based on sliding mode observer (SMO). Simulation results demonstrates advantages of this AAG guidance with the estimation approach based on SMO by comparing with the conventional guidance techniques and extended Kalman filter.

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Periodical:

Applied Mechanics and Materials (Volumes 110-116)

Pages:

5249-5256

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.110-116.5249

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Cite this paper

Online since:

October 2011

Authors:

Yuan Yun Song, Wan Chun Chen, Xing Liang Yin

Keywords:

Angular Acceleration Guidance, Extended Kalman Flter (EKF), Filter, Guidance Law, Sliding Mode Observer (SMO)

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References

[1] Paul Zarchan, Tactical and strategic missile guidance, American Institute of Aeronautics and Astronatics, Inc., Vol. 176, (1990).

Google Scholar

[2] George E, Observers in control systems, USA: Elsevier Academic Press, (2002).

Google Scholar

[3] K. Young, V. I. Utkin, A control engineer's guide to sliding mode control, IEEE Transaction on Control System Technology, Vol. 7, No. 3 , 1999, pp.212-232.

Google Scholar

[4] B. L. Walcott, M. J. Corless, S. H. Zak, Comparative study of monlinear state-observation techniques, Int. Jour. of Control, Vol. 45, 1987, pp.2109-2132.

DOI: 10.1080/00207178708933870

Google Scholar

[5] J. J. E. Slotine, J. K. Hedrick, E. A. Misawa, Nonlinear State Estimation Using Sliding Observers, Proceedings of 25th Conference on Decision and Control. Athens, Greece, 1986, pp.332-339.

DOI: 10.1109/cdc.1986.267257

Google Scholar

[6] K. R. Babu, I. G. Sarma, K. N. Swamy, Two Robust Homing Missile Guidance Laws Based on Sliding Mode Control Theory, Proceedings of NAECON, 1994, pp.540-547.

DOI: 10.1109/naecon.1994.332858

Google Scholar