Journal of System Simulation
Abstract
Abstract: The problem of designing a three-dimensional nonlinear guidance law accounting for saturation nonlinearity is concentrated to attack maneuvering targets. To solve the physical constraints of missile actuators, an anti-disturbance and anti-saturation terminal sliding mode guidance law is provided based on radial basis functions neural networks and adaptive method. The guidance law is bounded and ensures that the system state is uniformly ultimately bounded. Compared with the traditional anti-saturation guidance law, it has the advantages of fast convergence speed and high precision. Numerical simulations are introduced to demonstrate the effectiveness and superiority of the designed composite guidance law in theory.
Recommended Citation
Si, Yujie; Hua, Xiong; and Li, Zhe
(2021)
"Three-dimensional Adaptive Neural Network Guidance Law against Maneuvering Targets,"
Journal of System Simulation: Vol. 33:
Iss.
2, Article 23.
DOI: 10.16182/j.issn1004731x.joss.19-0434
Available at:
https://dc-china-simulation.researchcommons.org/journal/vol33/iss2/23
First Page
453
Revised Date
2020-05-17
DOI Link
https://doi.org/10.16182/j.issn1004731x.joss.19-0434
Last Page
460
CLC
TP391.9
Recommended Citation
Si Yujie, Xiong Hua, Li Zhe. Three-dimensional Adaptive Neural Network Guidance Law against Maneuvering Targets[J]. Journal of System Simulation, 2021, 33(2): 453-460.
DOI
10.16182/j.issn1004731x.joss.19-0434
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