@inproceedings{5225314a36ab44f4b046e816269a7909,
title = "Trajectory Tracking of a Quadrotor Missile via Adaptive Backstepping Control",
abstract = "This paper gives the mathematical model of a new aircraft named quadrotor missile and then proposes an effective nonlinear adaptive backstepping controller which combines the backstepping control technique and adaptive control technique. The controller can be devided into an inner attitude control loop and an outer position control loop, which are both using the adaptive backstepping control strategy to guarantee its convergence of Euler angles and position tracking. The asymptotic stability of the closed-loop system can be proved by Lyapunov analysis. Numerical simulations demonstrate this control strategy is capable of guaranteeing path tracking with desired attitude angles.",
keywords = "Adaptive control, Backstepping control, Lyapunov stability analysis, Path tracking",
author = "Huajie Zhu and Zhongjiao Shi and Liangyu Zhao",
note = "Publisher Copyright: {\textcopyright} 2022 IEEE.; 37th Youth Academic Annual Conference of Chinese Association of Automation, YAC 2022 ; Conference date: 19-11-2022 Through 20-11-2022",
year = "2022",
doi = "10.1109/YAC57282.2022.10023855",
language = "English",
series = "Proceedings - 2022 37th Youth Academic Annual Conference of Chinese Association of Automation, YAC 2022",
publisher = "Institute of Electrical and Electronics Engineers Inc.",
pages = "1420--1426",
booktitle = "Proceedings - 2022 37th Youth Academic Annual Conference of Chinese Association of Automation, YAC 2022",
address = "United States",
}