Open Access
ARTICLE
Intelligent Control for Integrated Guidance and Control Based on the Intelligent Characteristic Model
Jun Zhou, Zhenzhen Ge
Institute of Precision Guidance and Control, Northwestern Polytechnical University, Xi’an, China
* Corresponding Author: Zhenzhen Ge,
Intelligent Automation & Soft Computing 2018, 24(3), 623-631. https://doi.org/10.31209/2018.100000029
Abstract
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 first 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 proven using the Lyapunov stability theory. Finally, the
effectiveness of the adaptive IGC scheme is demonstrated using nonlinear numerical
simulations for the maneuvering target.
Keywords
Cite This Article
J. Zhou and Z. Ge, "Intelligent control for integrated guidance and control based on the intelligent characteristic model,"
Intelligent Automation & Soft Computing, vol. 24, no.3, pp. 623–631, 2018.