@inproceedings{35804a5e9fbd4b9aa6be2c354bc664c3,
title = "Guidance with terminal impact angular constraint for hybrid BTT/STT flight vehicle",
abstract = "Guidance law to guide the unpowered flight vehicle to attack ground target vertically is needed in modem warfare, and hybrid BTT/STT guidance command allocation is also needed to reduce the response time of the guidance system. A guidance law design method based on Lyapunov stability theory is proposed, and a guidance law with sight angle and sight angle velocity as feedback variables is designed in longitudinal plane of the vehicle motion. A guidance law aiming at eliminating lateral position error is based the same method is also presented. Guidance command allocation method based on the overload command and current bank angle is proposed to reduce the response time of the guidance system.",
keywords = "Angular Constraints, Bank to Turn, Guidance, Skip to Turn",
author = "Tao Chao and Songyanf Wang and Ming Yang",
note = "Publisher Copyright: {\textcopyright} 2014 TCCT, CAA.; Proceedings of the 33rd Chinese Control Conference, CCC 2014 ; Conference date: 28-07-2014 Through 30-07-2014",
year = "2014",
month = sep,
day = "11",
doi = "10.1109/ChiCC.2014.6896689",
language = "英语",
series = "Proceedings of the 33rd Chinese Control Conference, CCC 2014",
publisher = "IEEE Computer Society",
pages = "583--588",
editor = "Shengyuan Xu and Qianchuan Zhao",
booktitle = "Proceedings of the 33rd Chinese Control Conference, CCC 2014",
address = "美国",
}