@inproceedings{6e5c1953f2bc4273a7356dcd8d85b279,
title = "Orbital interception correction based on impulsive control",
abstract = "In this paper, orbit interception correction strategy using fixed-time constraints is considered. This work developed an optimal method for the problem based on the linear quadratic with discrete-time impulsive control. The linearized model was set up using the perturbation guidance equation, and the control system model was simplified. The control strategy was obtained by discrete impulsive optimization based on the discrete Dynamic Programming method. The calculation for the controller was extended. A numerical case was simulated to validate the control strategy's effectiveness. Since the simplified model and control method is easy to calculate, it is suitable for engineering application in midcourse interception guidance.",
keywords = "Discrete impulsive, Impulsive control, Interception correction, Linear quadratic optimal",
author = "Dongfang Chen and Yuancan Huang",
note = "Publisher Copyright: {\textcopyright} 2014 IEEE.; International Conference on Mechatronics and Control, ICMC 2014 ; Conference date: 03-07-2014 Through 05-07-2014",
year = "2015",
month = aug,
day = "31",
doi = "10.1109/ICMC.2014.7231630",
language = "English",
series = "Proceedings - 2014 International Conference on Mechatronics and Control, ICMC 2014",
publisher = "Institute of Electrical and Electronics Engineers Inc.",
pages = "623--627",
booktitle = "Proceedings - 2014 International Conference on Mechatronics and Control, ICMC 2014",
address = "United States",
}