H∞ hovering and guidance control for autonomous small-scale unmanned helicopter

9Citations
Citations of this article
7Readers
Mendeley users who have this article in their library.

Abstract

This paper describes hovering and horizontal guidance control with H ∞ controller and performance verification through flight experiments for the hobby-class small-scale unmanned helicopter. Simple system identification method was applied to acquire single-input/single-output models. Cross-validation results have shown that those models were reflected in the actual dynamics very well. Attitude control has been constructed by proportional-integral feedback loop with derivative feed-forward compensator for improvement of reference following performance. H∞ control theory was applied for horizontal velocity control. Four closed-loop transfer functions were shaped according to the design specifications given in the frequency domain. Also, horizontal position control has been designed as proportional-derivative feedback. In the flight experiment, good performance of hovering and reference following has been shown through 15 m square point-to-point traveling guidance control, and this also showed high accuracy of the models.

Cite

CITATION STYLE

APA

Fujiwara, D., Shin, J., Hazawa, K., & Nonami, K. (2004). H∞ hovering and guidance control for autonomous small-scale unmanned helicopter. Nippon Kikai Gakkai Ronbunshu, C Hen/Transactions of the Japan Society of Mechanical Engineers, Part C, 70(6), 1708–1714. https://doi.org/10.1299/kikaic.70.1708

Register to see more suggestions

Mendeley helps you to discover research relevant for your work.

Already have an account?

Save time finding and organizing research with Mendeley

Sign up for free