@inproceedings{c736ae6805b648d1b1b066e7b099a542,
title = "Decoupling control for hovering flight vehicle with parameter uncertainties",
abstract = "This paper proposes a new approach to consider nonlinear H ∞ control of hovering vehicles described by six-degree-of-freedom nonlinear dynamics with plant uncertainties due to the variation of moments of inertia caused by fuel consumption and/or payload operation. Taking into account nonlinear effect, plant uncertainty, and exogenous disturbances caused by wind gust, we show in this paper that the six-degree-of-freedom nonlinear H∞ controller can be exactly decoupled into two three-degree-of-freedom controllers, one for translational motion and the other for rotational motion, even though longitudinal and lateral dynamics of flight vehicle in hover are highly nonlinear and severely coupled.",
author = "Yang, {Ciann Dong} and Liu, {Wen Hsiung} and Chang, {Po Wei} and Weng, {Hung Jen}",
year = "2006",
month = jan,
day = "1",
doi = "10.2514/6.2006-6091",
language = "English",
isbn = "1563478196",
series = "Collection of Technical Papers - AIAA Guidance, Navigation, and Control Conference 2006",
publisher = "American Institute of Aeronautics and Astronautics Inc.",
pages = "786--798",
booktitle = "Collection of Technical Papers - AIAA Guidance, Navigation, and Control Conference 2006",
note = "AIAA Guidance, Navigation, and Control Conference 2006 ; Conference date: 21-08-2006 Through 24-08-2006",
}