Autosoft Journal

Online Manuscript Access

Intelligent Control for Integrated Guidance and Control based on Intelligent Characteristic Model


In this paper, an adaptive integrated guidance and control (IGC) scheme for the homing missile is proposed based on the novel continuous characteristic model and the dynamic surface control technique. The novel continuous characteristic model is firstly proposed in the presence of unknown model coefficients and uncertainties. Then, the dynamic surface control technique is applied to the continuous characteristic model. The proposed IGC scheme guarantees the line-of-sight angular rates converge to an arbitrarily small neighbourhood of zero and all the closed-loop signals to be semi-globally uniformly ultimately bounded, which is proved using the Lyapunov stability theory. Finally, the effectiveness of the adaptive IGC scheme is demonstrated using nonlinear numerical simulations for the maneuvering target.



Total Pages: 10
Pages: 623-632


Manuscript ViewPdf Subscription required to access this document

Obtain access this manuscript in one of the following ways

Already subscribed?

Need information on obtaining a subscription? Personal and institutional subscriptions are available.

Already an author? Have access via email address?


Volume: 24
Issue: 3
Year: 2018

Cite this document


G.M. Dimirovski, Y.W. Jing, W.L. Li, & X.P. Liu. (2006). Adaptive back-stepping design of TCSC robust nonlinear control for power systems, Intelligent Automation and Soft Computing. 12(1), 75-87.

H. Huang, & Z. Zhang. (2015). Characteristic model-based H2/H∞ robust adaptive control during the re-entry of hypersonic cruise vehicles, Science China Information Sciences. 58(1), 012202.

M. Z. Hou, X.L. Liang, & G.R. Duan. (2013). Adaptive block dynamic surface control for integrated missile guidance and autopilot, Chinese Journal of Aeronautics. 26(3), 741-750.

A. S. Kendrick Y. Lin, & A.B. Waseem. (2013). Adaptive dynamic surface control for a class of MIMO nonlinear systems with actuator failures, International Journal of Systems Science. 44(3), 479-492.

X. L. Liang, M.Z. Hou, & G. R. Duan. (2015). Adaptive dynamic surface control for integrated missile guidance and autopilot in the presence of input saturation, Journal of Aerospace Engineering. 28(5), 04014121.

P. K. Menon, G. D. Sweriduk, E.J. Ohlmeyer, & D. S. Malyevac. (2004). Integrated guidance and control of moving mass actuated kinetic warheads, Journal of Guidance Control and Dynamics. 27(1), 118-126.

R. Padhi, C. Chawla, & P.G. Das. (2014). Partial integrated guidance and control of interceptors for high-speed ballistic targets, Journal of Guidance Control and Dynamics. 37(1), 149-163.

H. T. Song & T. Zhang. (2016). Fast robust integrated guidance and control design of interceptors, IEEE Transactions on Control Systems Technology. 24(1), 349-356.

M. C. Song, Y. Lin, & R. Huang. (2014). Robust adaptive dynamic surface control for linear time-varying systems, International Journal of Adaptive Control and Signal Processing. 28, 932-948.

C.L. Wang & Y. Lin. (2010). Adaptive dynamic surface control for linear multivariable systems, Automatica. 46(10), 1703-1711.

X. F. Wang, Y.Y. Zheng, & H. Lin. (2015). Integrated guidance and control law for cooperative attack of multiple missiles, Aerospace Science and Technology. 42, 1-11.

X. H. Wang, & J. Z. Wang. (2014). Partial integrated guidance and control for missiles with three-dimensional impact angle constraints, Journal of Guidance Control and Dynamics. 37(2), 644-657.

W.H. Wang, S.F. Xiong, S. Wang, S. Y. Song, & C. Lai. (2016). Three dimensional impact angle constrained integrated guidance and control for missiles with input saturation and actuator failure, Aerospace Science and Technology. 53, 169-187.

H.X. Wu, J. Hu, & Y.C. Xie. (2007). Characteristic model-based all-coefficient adaptive control method and its applications, IEEE Transactions on Systems Man and Cybernetics Part C: Applications and Reviews. 37(2), 213-221.

S. S. Vaddi, P. K. Menon, & E. J. Ohlmeyer. (2009). Numerical state-dependent Riccati equation approach for missile integrated guidance control, Journal of Guidance Control and Dynamics. 32(2), 699-703.

H. Yan & H.B. Ji. (2012). Integrated guidance and control for dual-control missiles based on small-gain theorem, Automatica. 48(10), 2686-2692.

H. Yan, X.H. Wang, B.F. Yu, & H.B. Ji. (2014). Adaptive integrated guidance and control based on backstepping and input-to-state stability, Asian Journal of Control. 16(2), 602-608.

C. Zhang & Y.J. Wu, (2016). Dynamic surface control and active disturbance rejection control-based integrated guidance and control design and simulation for hypersonic reentry missile, International Journal of Modeling Simulation and Scientific Computing. 7(3), 1650025.

Z. Zhang & J. Hu. (2012). Stability analysis of a hypersonic vehicle controlled by the characteristic model based adaptive controller, Science China Information Sciences. 55(10), 2243-2256.


ISSN PRINT: 1079-8587
ISSN ONLINE: 2326-005X
DOI PREFIX: 10.31209
10.1080/10798587 with T&F
IMPACT FACTOR: 0.652 (2017/2018)
Journal: 1995-Present

SCImago Journal & Country Rank


TSI Press
18015 Bullis Hill
San Antonio, TX 78258 USA
PH: 210 479 1022
FAX: 210 479 1048