@inproceedings{0a1129be2cb44b4da58169ba2cd0fe05,
title = "A fast-online guidance method for trajectory correction projectiles",
abstract = "The fast-online guidance problem of trajectory correction projectile is investigated in this paper. The dynamic mathematical model of spin-stability projectile is briefly presented and a simplified process for the nonlinear seven degree of freedom model is given in detail. Then a linear approximate model is introduced to calculate trim points along the projectile trajectory, and the trajectory characteristics is given through the trim results. A real-time method for calculating the control angle of the course correction fuse is also proposed base on the above trim method. Finally, simulation results are given to validate the proposed method.",
keywords = "Course correction fuse, Flight control, Spin-stability projectile, Trajectory correction",
author = "Yuhan Mou and Jing Zhang and Lingyu Yang and Xiaoke Feng",
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.2019.8865246",
language = "英语",
series = "Chinese Control Conference, CCC",
publisher = "IEEE Computer Society",
pages = "3970--3975",
editor = "Minyue Fu and Jian Sun",
booktitle = "Proceedings of the 38th Chinese Control Conference, CCC 2019",
address = "美国",
}