Optimization Maneuver Strategy which Make the Loss of Height of UAV Minimum after Engine Stopped

Kai Wang; Chun Zhen Sun; Yi Jiang

doi:10.4028/www.scientific.net/AMM.668-669.619

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HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vols. 668-669Optimization Maneuver Strategy which Make the Loss...

Optimization Maneuver Strategy which Make the Loss of Height of UAV Minimum after Engine Stopped

Abstract:

This paper researches optimization maneuver strategy of UAV after engine stopped to make the loss of height of UAV minimum. Research has been done in two conditions, unpowered balanced glide straight flight and unpowered balanced glide turn maneuver. In this paper, the angle of attack and angle of roll has been given in order to make sure that the loss of the height is a minimum. The results of the simulations show that the optimization maneuver strategy in this paper is correct.

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Periodical:

Applied Mechanics and Materials (Volumes 668-669)

Pages:

619-624

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.668-669.619

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Cite this paper

Online since:

October 2014

Authors:

Kai Wang*, Chun Zhen Sun, Yi Jiang

Keywords:

Engine Stopped, Optimization Maneuver Strategy, Shipboard UAV

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* - Corresponding Author

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