@inproceedings{70507dd0759f4ade8ba537f40aa96b91,
title = "Swing control of helicopter sling load by using command smoothing technique",
abstract = "Motion-induced oscillations of helicopter sling load seriously degrade their effectiveness and safety. The modeling and dynamics of helicopter sling load are derived. A novel control scheme is designed for reducing the payload swing. Simulations of a large range of motions and various system parameters are used to analyze the dynamic behavior and the robustness of the control scheme. Experimental results obtained from a model helicopter sling load validate the simulated dynamic behavior and the effectiveness of the control scheme.",
keywords = "Command Smoothing, Helicopter Sling Load, Swing Control",
author = "Haining Wang and Jie Huang",
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.2014.6896335",
language = "English",
series = "Proceedings of the 33rd Chinese Control Conference, CCC 2014",
publisher = "IEEE Computer Society",
pages = "7988--7993",
editor = "Shengyuan Xu and Qianchuan Zhao",
booktitle = "Proceedings of the 33rd Chinese Control Conference, CCC 2014",
address = "United States",
}