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Mathematical modeling of helicopter aerobatic maneuvers

Yihua Cao (Department of Flight Vehicle Design and Applied Mechanics, Beijing University of Aeronautics and Astronautics, Beijing, People’s Republic of China)
Guangli Zhang (Department of Flight Vehicle Design and Applied Mechanics, Beijing University of Aeronautics and Astronautics, Beijing, People’s Republic of China)
Yuan Su (Department of Flight Vehicle Design and Applied Mechanics, Beijing University of Aeronautics and Astronautics, Beijing, People’s Republic of China)

Aircraft Engineering and Aerospace Technology

ISSN: 0002-2667

Article publication date: 1 April 2004

1035

Abstract

This paper describes the typical maneuvering courses of helicopters with mathematics systematically and presents the formulas and approaches for calculating the dynamics characteristics. A set of generalized equations which govern the kinematics and dynamics of helicopters in maneuvering flight is given. Three aerobatic maneuvers for loop, roll and turn are specially analyzed in detail and the sample calculations are presented. The method established in this paper is of practical significance for aerobatic employment and design of helicopters.

Keywords

Citation

Cao, Y., Zhang, G. and Su, Y. (2004), "Mathematical modeling of helicopter aerobatic maneuvers", Aircraft Engineering and Aerospace Technology, Vol. 76 No. 2, pp. 170-178. https://doi.org/10.1108/00022660410526033

Publisher

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Emerald Group Publishing Limited

Copyright © 2004, Emerald Group Publishing Limited

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