Design of Optimal Control for a Stratospheric Airship Based on Generalized Coordinate Frame

Ming Zhu; Yong Mei Wu; Ze Wei Zheng

doi:10.4028/www.scientific.net/AMR.466-467.587

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HomeAdvanced Materials ResearchAdvanced Materials Research Vols. 466-467Design of Optimal Control for a Stratospheric...

Design of Optimal Control for a Stratospheric Airship Based on Generalized Coordinate Frame

Abstract:

An optimal control is presented in this paper. First, nonlinear dynamic model of a six degree of freedom stratospheric airship, traditional and full-actuated, is built based on generalized coordinate frame. Second, optimal control law is determined by Hamilton function and performance index function. This optimal control can be regarded as extension of feedback linearization control law.

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Periodical:

Advanced Materials Research (Volumes 466-467)

Pages:

587-591

DOI:

https://doi.org/10.4028/www.scientific.net/AMR.466-467.587

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Online since:

February 2012

Authors:

Ming Zhu, Yong Mei Wu, Ze Wei Zheng

Keywords:

Generalized Coordinate Frame, Optimal Control, Stratospheric Airship

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References

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