@inproceedings{0dd62b48689b4d3ea9173adcec9c157b,
title = "Design of missile longitudinal control system based on backstepping control",
abstract = "Missile control system is not block strict feedback system which is suitable to use backstepping method. So in this paper, a backstepping control method is proposed to design a missile longitudinal autopilot and is proved to be asymptotically stable by Lyapunov stability theory. The simulation results show that the designed system can still track commands quickly and accurately and is robust with aerodynamic perturbation and control input saturation.",
keywords = "Aerodynamic parameters perturbation, Backstepping control, Input saturation, Missile longitudinal autopilot",
author = "Li, {Mei Hong} and Jian Yin and Sun, {Xue Yang} and Xu, {Jin Xiang} and Zhang, {Mei Mei}",
year = "2014",
doi = "10.4028/www.scientific.net/AMM.496-500.1401",
language = "English",
isbn = "9783037859926",
series = "Applied Mechanics and Materials",
pages = "1401--1406",
booktitle = "Frontiers of Manufacturing and Design Science IV",
note = "4th International Conference on Frontiers of Manufacturing and Design Science, ICFMD 2013 ; Conference date: 10-09-2013 Through 12-09-2013",
}