Journal of System Simulation
Abstract
Abstract: The strong coupling of the hypersonic vehicle, the high order of the model, and the perturbation of the aerodynamic parameters make it difficult for the general controller to achieve the desired control effect. The self-disturbing tandem technique can well meet the requirements of the high-order model control. The use of sliding mode variable structure technology which is not sensitive to perturbation of parameters can enhance the system immunity. The simulation results show that the control effect is very good.
Recommended Citation
Cheng, Mingzhi; Wu, Yunjie; and Fei, Ma
(2020)
"Sliding Mode Auto - Disturbance Rejection Control of Hypersonic Vehicle under Disturbance,"
Journal of System Simulation: Vol. 29:
Iss.
10, Article 21.
DOI: 10.16182/j.issn1004731x.joss.201710021
Available at:
https://dc-china-simulation.researchcommons.org/journal/vol29/iss10/21
First Page
2391
DOI Link
https://doi.org/10.16182/j.issn1004731x.joss.201710021
Last Page
2397
CLC
TP391.9
Recommended Citation
Cheng Mingzhi, Wu Yunjie, Ma Fei. Sliding Mode Auto - Disturbance Rejection Control of Hypersonic Vehicle under Disturbance[J]. Journal of System Simulation, 2017, 29(10): 2391-2397.
DOI
10.16182/j.issn1004731x.joss.201710021
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