@inproceedings{02a7b2bcc8644975a82623dece0d1fa0,
title = "Design of full-envelope flight control based on the MDADT",
abstract = "With the regarding to the demand that the parameters vary rapidly over a wide range for the highly maneuverable technology (HiMAT) vehicle, a switched linear model with the locally overlapped characteristic is established for a full-envelope flight. Based on the mode-dependent average dwell time (MDADT) method, a stability criterion for the above switched linear model is proposed, and an application to a full-envelope flight controller is designed, which shows fewer restrictions than that of the average dwell time (ADT). Furthermore, a numerical simulation is given to prove the correctness and feasibility of this method.",
keywords = "HiMAT, MDADT, full-envelope flight controller, stability criterion, switched linear system",
author = "Qing Wang and Xiaohui Liang and Chaoyang Dong",
note = "Publisher Copyright: {\textcopyright} 2017 Technical Committee on Control Theory, CAA.; 36th Chinese Control Conference, CCC 2017 ; Conference date: 26-07-2017 Through 28-07-2017",
year = "2017",
month = sep,
day = "7",
doi = "10.23919/ChiCC.2017.8027337",
language = "英语",
series = "Chinese Control Conference, CCC",
publisher = "IEEE Computer Society",
pages = "157--163",
editor = "Tao Liu and Qianchuan Zhao",
booktitle = "Proceedings of the 36th Chinese Control Conference, CCC 2017",
address = "美国",
}