@inproceedings{22a8691c0fc04f8ba311165f939d5f6d,
title = "Reference command tracking and simulation research of hypersonic cruise vehicle",
abstract = "The focus of this paper is on control design and simulation for an air-breathing hypersonic cruise vehicle (HCV). Aiming at the highly nonlinear and strong coupling for HCV mathematical model, the theory of feedback linearization based Lie derivative introduced can convert accurately nonlinear mathematic model into equivalent linear model for control design. By the proper transformation, dynamic inversion flight control systems for hypersonic vehicle designed can stabilize the system and relieve the coupling effects. Simulation results show the correctness of the simulation platform and the effectiveness of the control approach.",
keywords = "Dynamic inversion, Hypersonic cruise vehicle, Linearization, Tracking control",
author = "Chengbin Lian and Zhang Ren and Xinyue Shao",
year = "2012",
doi = "10.1049/cp.2012.1300",
language = "英语",
isbn = "9781849195379",
series = "IET Conference Publications",
number = "598 CP",
pages = "1642--1646",
booktitle = "International Conference on Automatic Control and Artificial Intelligence, ACAI 2012",
edition = "598 CP",
note = "International Conference on Automatic Control and Artificial Intelligence, ACAI 2012 ; Conference date: 03-03-2012 Through 05-03-2012",
}