@inproceedings{3af9c696ec994355998321ac49ee7982,
title = "Super-maneuver control of thrust vector aircraft based on nonlinear dynamic inversion",
abstract = "Thrust vector control method refers to the technology that the thrust component produced by the deflection of the nozzle or tail jet can replace the control surface of the original aircraft or enhance the control function of the aircraft and control the flight of the aircraft in real time. The greatest technical potential of thrust vector is that it can significantly improve the post-stall maneuverability of aircraft, thus greatly improving the combat effectiveness and survivability of aircraft. Based on the aircraft control system, this paper builds a multiple control plane model in SIMULINK, uses the nonlinear dynamic inversion theory to control the allocation design, and studies the aircraft thrust vector control allocation method.",
keywords = "Nonlinear dynamic inversion, Super-maneuver, Thrust vector",
author = "Yongfeng Li and Weiguo Zhang and Jingping Shi",
note = "Publisher Copyright: {\textcopyright} 2019 Technical Committee on Control Theory, Chinese Association of Automation.; 38th Chinese Control Conference, CCC 2019 ; Conference date: 27-07-2019 Through 30-07-2019",
year = "2019",
month = jul,
doi = "10.23919/ChiCC.2019.8866051",
language = "英语",
series = "Chinese Control Conference, CCC",
publisher = "IEEE Computer Society",
pages = "8031--8036",
editor = "Minyue Fu and Jian Sun",
booktitle = "Proceedings of the 38th Chinese Control Conference, CCC 2019",
}