@inproceedings{d1f8dc8649b44ed09c35d3b2418f2858,
title = "A Maneuvering Penetration Guidance Law Based on Variable Structure Control",
abstract = "As an important penetration technique, the design of penetration trajectory has been widely studied. However, how to design the corresponding guidance law to implement the maneuvering trajectory has rarely been considered in literature. Therefore, a sliding mode guidance for trajectory maneuvering is designed in this paper, in which the inertia lag of autopilot is considered and the line-of-sight rate is forced to track a given sinusoidal signal. Theoretical analysis shows that the designed maneuvering guidance law can drive the system to a sliding surface, where the tracking error is zero. Simulation results show that the proposed guidance law has good accuracy and robustness considering parameter perturbation and external environment disturbance.",
keywords = "autopilot inertia, guidance law, maneuvering penetration, variable structure control",
author = "Zhuonan Liang and Fenfen Xiong",
note = "Publisher Copyright: {\textcopyright} 2020 Technical Committee on Control Theory, Chinese Association of Automation.; 39th Chinese Control Conference, CCC 2020 ; Conference date: 27-07-2020 Through 29-07-2020",
year = "2020",
month = jul,
doi = "10.23919/CCC50068.2020.9188502",
language = "English",
series = "Chinese Control Conference, CCC",
publisher = "IEEE Computer Society",
pages = "2067--2071",
editor = "Jun Fu and Jian Sun",
booktitle = "Proceedings of the 39th Chinese Control Conference, CCC 2020",
address = "United States",
}