Non-singular Terminal Sliding Mode Control for Bank-to-Turn Missile Based on Active Disturbance Rejection Decoupling Controller

Authors

Ma Fei, 1. State Key Laboratory of Virtual Reality Technology and System, Beihang University, Beijing 100191, China;;2. School of Automation Science and Electrical Engineering, Beihang University, Beijing 100191, China;;3. Science and Technology on Aircraft Control Laboratory, Beijing 100191, China;
Yunjie Wu, 1. State Key Laboratory of Virtual Reality Technology and System, Beihang University, Beijing 100191, China;;2. School of Automation Science and Electrical Engineering, Beihang University, Beijing 100191, China;;3. Science and Technology on Aircraft Control Laboratory, Beijing 100191, China;
Mingzhi Cheng, 1. State Key Laboratory of Virtual Reality Technology and System, Beihang University, Beijing 100191, China;;2. School of Automation Science and Electrical Engineering, Beihang University, Beijing 100191, China;;3. Science and Technology on Aircraft Control Laboratory, Beijing 100191, China;

Abstract

Abstract: An overload tracking model was established, based on the traditional model of BTT (Bank-to-Turn) missile, and an ADRDC (active disturbance rejection decoupling controller) was designed because of the strong coupling problem in this model. For the coupled channel, the decoupling was performed by the ADRDC, and then the NTSMC (non-singular terminal sliding mode controller) was added. For the non-coupled channel, only the NTSMC was designed. The experimental results show that the new control strategy can combine the strong robustness of ADRDC with the finite time convergence ability of NTSMC. Besides, it shows good dynamic performances and steady-state performance and is effective in tracking control.

Recommended Citation

Fei, Ma; Wu, Yunjie; and Cheng, Mingzhi (2020) "Non-singular Terminal Sliding Mode Control for Bank-to-Turn Missile Based on Active Disturbance Rejection Decoupling Controller," Journal of System Simulation: Vol. 29: Iss. 9, Article 41.
DOI: 10.16182/j.issn1004731x.joss.201709040
Available at: https://dc-china-simulation.researchcommons.org/journal/vol29/iss9/41

First Page

2175

DOI Link

https://doi.org/10.16182/j.issn1004731x.joss.201709040

Last Page

2181

CLC

TP273+.3

Recommended Citation

Ma Fei, Wu Yunjie, Cheng Mingzhi. Non-singular Terminal Sliding Mode Control for Bank-to-Turn Missile Based on Active Disturbance Rejection Decoupling Controller[J]. Journal of System Simulation, 2017, 29(9): 2175-2181.

DOI

10.16182/j.issn1004731x.joss.201709040