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

^*Corresponding author for this work

School of Aeronautic Science and Engineering

Beihang University

Research output: Contribution to journal › Article › peer-review

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.

Original language	English
Pages (from-to)	5787-5790+5794
Journal	Xitong Fangzhen Xuebao / Journal of System Simulation
Volume	20
Issue number	21
State	Published - 5 Nov 2008

Keywords

Escape
Flight path
Lateral
Longitudinal
Microburst
Nonlinear inverse dynamics
Simulation

Cite this

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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\}",

year = "2008",

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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

M3 - 文章

AN - SCOPUS:56849087431

SN - 1004-731X

VL - 20

SP - 5787-5790+5794

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

Abstract

Keywords

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