Longitudinal/lateral NID control of aircraft take-off path in windshear

Kun Gang Yuan; Yi Hua Cao

Longitudinal/lateral NID control of aircraft take-off path in windshear

Kun Gang Yuan^*
, Yi Hua Cao

^*此作品的通讯作者

航空科学与工程学院

Beihang University

科研成果: 期刊稿件 › 文章 › 同行评审

摘要

An axisymmetric, three-dimensional engineering model of microburst was used in the simulation of aircraft take-off with windshear encounter. The employed control law of longitudinal and lateral maneuver was built using nonlinear inverse dynamics (NID) method. The simulation flight parameters and microburst parameters of longitudinal and lateral maneuver were analyzed. The analysis results show that the aircraft flight performance and survival ability are more effective in lateral maneuver.

源语言	英语
页（从-至）	5787-5790+5794
期刊	Xitong Fangzhen Xuebao / Journal of System Simulation
卷	20
期	21
出版状态	已出版 - 5 11月 2008

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引用此

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title = "Longitudinal/lateral NID control of aircraft take-off path in windshear",

abstract = "An axisymmetric, three-dimensional engineering model of microburst was used in the simulation of aircraft take-off with windshear encounter. The employed control law of longitudinal and lateral maneuver was built using nonlinear inverse dynamics (NID) method. The simulation flight parameters and microburst parameters of longitudinal and lateral maneuver were analyzed. The analysis results show that the aircraft flight performance and survival ability are more effective in lateral maneuver.",

keywords = "Escape, Flight path, Lateral, Longitudinal, Microburst, Nonlinear inverse dynamics, Simulation",

author = "Yuan, \{Kun Gang\} and Cao, \{Yi Hua\}",

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T1 - Longitudinal/lateral NID control of aircraft take-off path in windshear

AU - Yuan, Kun Gang

AU - Cao, Yi Hua

PY - 2008/11/5

Y1 - 2008/11/5

N2 - An axisymmetric, three-dimensional engineering model of microburst was used in the simulation of aircraft take-off with windshear encounter. The employed control law of longitudinal and lateral maneuver was built using nonlinear inverse dynamics (NID) method. The simulation flight parameters and microburst parameters of longitudinal and lateral maneuver were analyzed. The analysis results show that the aircraft flight performance and survival ability are more effective in lateral maneuver.

AB - An axisymmetric, three-dimensional engineering model of microburst was used in the simulation of aircraft take-off with windshear encounter. The employed control law of longitudinal and lateral maneuver was built using nonlinear inverse dynamics (NID) method. The simulation flight parameters and microburst parameters of longitudinal and lateral maneuver were analyzed. The analysis results show that the aircraft flight performance and survival ability are more effective in lateral maneuver.

KW - Escape

KW - Flight path

KW - Lateral

KW - Longitudinal

KW - Microburst

KW - Nonlinear inverse dynamics

KW - Simulation

UR - https://www.scopus.com/pages/publications/56849087431

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SN - 1004-731X

VL - 20

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JO - Xitong Fangzhen Xuebao / Journal of System Simulation

JF - Xitong Fangzhen Xuebao / Journal of System Simulation

IS - 21

ER -

Longitudinal/lateral NID control of aircraft take-off path in windshear

摘要

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