Landing Performance Optimization Algorithm of Civil Aircrafts

Hong Ying Chen; Wen Tian Luo

doi:10.4028/www.scientific.net/AMM.253-255.2176

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HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vols. 253-255Landing Performance Optimization Algorithm of...

Landing Performance Optimization Algorithm of Civil Aircrafts

Abstract:

This paper explains and demonstrates how to calculate and optimize landing performance. According regulation requirement, it needs to consider the different requirements [1], including landing field length, missed approach climb gradient, brake energy and tire speed. Weights limited by the different requirements are calculated, the minimum of these weights limited are determined as the actual allowed maximum landing weight.

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Periodical:

Applied Mechanics and Materials (Volumes 253-255)

Pages:

2176-2180

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.253-255.2176

Citation:

Cite this paper

Online since:

December 2012

Authors:

Hong Ying Chen, Wen Tian Luo

Keywords:

Landing Performance, Landing Speed, Landing Weight, Operating Landing Distance, Optimization Algorithm

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References

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