2023
DOI: 10.1109/access.2023.3241484
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Design of Three-Dimensional Intelligent Guidance Law for Intercepting Highly Maneuvering Target

Abstract: This paper investigates the three-dimensional guidance and control problem of missile intercepting highly maneuvering target, whose acceleration information is difficult to accurately predict. With the three-dimensional guidance model for intercepting single target established by using the principle of zeroing the rate of line-of-sight (LOS), a novel intelligence guidance law has been designed through backstepping sliding mode control method, radial basis function (RBF) neural network and adaptive control tech… Show more

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Cited by 2 publications
(1 citation statement)
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“…Recently, neural networks (NNs) have been successfully applied in nonlinear system [6], especially for aerospace engineering [7], NN for steering law for manoeuvring targets [8], NN of missile guidance control [9]. Su et al presented a guidance law in [8], which was developed using the backstepping method of sliding mode control, a radial basis function (RBF) neural network, and an adaptive control technique. A Lyapunov-based stability analysis shows that all signals are bounded and the LOS rates eventually converge near the origin.…”
Section: Introductionmentioning
confidence: 99%
“…Recently, neural networks (NNs) have been successfully applied in nonlinear system [6], especially for aerospace engineering [7], NN for steering law for manoeuvring targets [8], NN of missile guidance control [9]. Su et al presented a guidance law in [8], which was developed using the backstepping method of sliding mode control, a radial basis function (RBF) neural network, and an adaptive control technique. A Lyapunov-based stability analysis shows that all signals are bounded and the LOS rates eventually converge near the origin.…”
Section: Introductionmentioning
confidence: 99%