@inproceedings{8fbbf0b168b549899c12d8d70e45c25c,
title = "LQR tracking guidance law for hypersonic vehicle",
abstract = "In order to study the reentry guidance law for hypersonic vehicle, the theory of linear quadratic regulator (LQR) is introduced into the solving process of guidance law based on a determined standard trajectory. Small disturbance linearization of complete three-degree-of-freedom (3DOF) model is carried out. Guidance command which satisfies the requirement of the mission can be obtained by using LQR method. Simulations are done by parameter deviating so as to verify the robustness of the algorithm. The results shows that the method of this paper can ensure high accuracy tracking of nominal trajectory and has strong robustness.",
keywords = "Hypersonic vehicle, LQR, Trajectory tracking",
author = "Qing Lu and Jun Zhou",
note = "Publisher Copyright: {\textcopyright} 2017 IEEE.; 29th Chinese Control and Decision Conference, CCDC 2017 ; Conference date: 28-05-2017 Through 30-05-2017",
year = "2017",
month = jul,
day = "12",
doi = "10.1109/CCDC.2017.7978461",
language = "英语",
series = "Proceedings of the 29th Chinese Control and Decision Conference, CCDC 2017",
publisher = "Institute of Electrical and Electronics Engineers Inc.",
pages = "7090--7094",
booktitle = "Proceedings of the 29th Chinese Control and Decision Conference, CCDC 2017",
}