Adaptive sliding mode control for missile guidance law

The problem of missile interception is investigated in this paper. Sliding mode controllers are proposed for the design of guidance laws. Specially, the control design consists of the estimation of the target acceleration by adaptive scheme and thus it achieves the decrease of undesired chattering effectively. Also, simulation results are presented to illustrate the effectiveness of the control strategies.

[1]  Andrey V. Savkin,et al.  Circular-Navigation-Guidance Law for Precision Missile/Target Engagements , 2006 .

[2]  Ciann-Dong Yang,et al.  Nonlinear H∞ Robust Guidance Law for Homing Missiles , 1998 .

[3]  Tal Shima,et al.  An LQG guidance law with bounded acceleration command , 2003, 42nd IEEE International Conference on Decision and Control (IEEE Cat. No.03CH37475).

[4]  Zhihong Man,et al.  Continuous finite-time control for robotic manipulators with terminal sliding mode , 2003, Autom..

[5]  Min-Jea Tahk,et al.  Guidance Synthesis for Evasive Maneuver of Anti-Ship Missiles Against Close-In Weapon Systems , 2010, IEEE Transactions on Aerospace and Electronic Systems.

[6]  Dongkyoung Chwa,et al.  Adaptive nonlinear guidance law considering control loop dynamics , 2003 .

[7]  H. Weiss,et al.  LQC guidance law with bounded acceleration command , 2008, IEEE Transactions on Aerospace and Electronic Systems.

[8]  Chih-Min Lin,et al.  Guidance Law Design by Adaptive Fuzzy Sliding-Mode Control , 2002 .

[9]  Dong Xu,et al.  Missile Guidance Law Based on Extended State Observer , 2013, IEEE Transactions on Industrial Electronics.

[10]  K. Teo,et al.  Guidance Laws with Finite Time Convergence , 2009 .

[11]  A. Levant,et al.  Guidance and Control of Missile Interceptor using Second-Order Sliding Modes , 2009, IEEE Transactions on Aerospace and Electronic Systems.

[12]  Yuri Ulybyshev.  Terminal Guidance Law Based on Proportional Navigation , 2005 .

[13]  Dennis S. Bernstein,et al.  Finite-Time Stability of Continuous Autonomous Systems , 2000, SIAM J. Control. Optim..

[14]  Chang-Hun Lee,et al.  Polynomial Guidance Laws Considering Terminal Impact Angle and Acceleration Constraints , 2013, IEEE Transactions on Aerospace and Electronic Systems.

[15]  Youdan Kim,et al.  Circular Motion Guidance Law for Coordinated Standoff Tracking of a Moving Target , 2013, IEEE Transactions on Aerospace and Electronic Systems.

[16]  Haim Weiss,et al.  Stochastic Approach to Optimal Guidance with Uncertain Intercept Time , 2010, IEEE Transactions on Aerospace and Electronic Systems.

[17]  Youdan Kim,et al.  Design of Missile Guidance Law via Variable Structure Control , 2000 .

[18]  Y. Stepanenko,et al.  A sliding mode controller with improved adaptation laws for the upper bounds on the norm of uncertainties , 1996, Proceedings. 1996 IEEE International Workshop on Variable Structure Systems. - VSS'96 -.