@inproceedings{e045edb5dace4e24b35b55bc4b2fcb82,
title = "Dynamic Inversion controller design for BTT Missile Based on Sliding Mode control",
abstract = "Aiming at nonlinear BBT control problem with uncertainty and serious coupled, this paper adopts dynamic inversion theory and sliding mode theory. Firstly, the control system was divided into slow loop and fast loop based on the singular value perturbation theory. Then dynamic inversion control method is applied for both two loops. The sliding mode control is adopted to overcome the inverse error caused by inaccuracy of model and parameter perturbation. The control law of slow loop is given and stability of close loop system is proved. Finally, the performance and robustness of the designed controller are verified by simulation.",
keywords = "BTT missile, autopilot, dynamic inversion control, sliding mode control",
author = "Bin Huang and Yongshan Liu and Anran Xu",
note = "Publisher Copyright: {\textcopyright} 2021 IEEE.; 4th IEEE Advanced Information Management, Communicates, Electronic and Automation Control Conference, IMCEC 2021 ; Conference date: 18-06-2021 Through 20-06-2021",
year = "2021",
month = jun,
day = "18",
doi = "10.1109/IMCEC51613.2021.9482013",
language = "English",
series = "IMCEC 2021 - IEEE 4th Advanced Information Management, Communicates, Electronic and Automation Control Conference",
publisher = "Institute of Electrical and Electronics Engineers Inc.",
pages = "1820--1824",
editor = "Bing Xu",
booktitle = "IMCEC 2021 - IEEE 4th Advanced Information Management, Communicates, Electronic and Automation Control Conference",
address = "United States",
}