@inproceedings{0f6e32e592d44285afd15d41cf5e61e4,
title = "LPV-MRAC Method for Aircraft with Structural Damage",
abstract = "Abrupt structural damage poses significant challenges to the flight safety and flight quality of aircraft. In this paper, a direct model reference adaptive control (MRAC) method based on a linear parameter-varying (LPV) model is proposed to recover the control performance and flight quality of damaged aircraft. The design of the controller is based on a polytopic LPV model and the higher order singular value decomposition (HOSVD) model reduction method to reduce the computational cost of identifying the damaged aircraft model. The proposed controller also extends a previous MRAC method which assumes the input matrix is unchanged for different damage cases by identifying an uncertain input parameter online. The developed LPV-MRAC method is validated by simulation on NASA's generic transport model (GTM) with left wing tip loss damage and shown to be capable of compensating the damage effects and restoring the aircraft's control performance shortly after the damage. The flight quality of the closed-loop damaged aircraft is also evaluated by the C-star criterion and shown to be within Class I under the proposed controller.",
keywords = "Aircraft with structural damage, Model reference adaptive control, Polytopic LPV models, Uncertainty of input matrix",
author = "Bo Peng and Lingyu Yang and Xiaoke Yang",
note = "Publisher Copyright: {\textcopyright} 2016 TCCT.; 35th Chinese Control Conference, CCC 2016 ; Conference date: 27-07-2016 Through 29-07-2016",
year = "2016",
month = aug,
day = "26",
doi = "10.1109/ChiCC.2016.7553859",
language = "英语",
series = "Chinese Control Conference, CCC",
publisher = "IEEE Computer Society",
pages = "3262--3267",
editor = "Jie Chen and Qianchuan Zhao and Jie Chen",
booktitle = "Proceedings of the 35th Chinese Control Conference, CCC 2016",
address = "美国",
}