Modelling and simulation of an aerial vehicle steering to hit on top of the target at terminal trajectory

Zheng Jie Wang; Ning Jun Fan; Jing Lu

doi:10.1504/IJAMECHS.2011.042612

Modelling and simulation of an aerial vehicle steering to hit on top of the target at terminal trajectory

Zheng Jie Wang^*, Ning Jun Fan, Jing Lu

^*Corresponding author for this work

School of Mechatronical Engineering

Beijing Institute of Technology

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

Abstract

In this paper, combined attitude control of the terminal trajectory for an aerial vehicle is presented. The combined attitude controller includes the fuzzy adaptive aerodynamic force mode control and the direct lateral thrust mode control. The dynamic and kinematics mathematical models of the aerial vehicle are built based on the designed reaction-jet control scheme. Simulation results show that the combined control system can satisfy the requirements of the aerial vehicle overload better than the traditional mode does.

Original language	English
Pages (from-to)	159-167
Number of pages	9
Journal	International Journal of Advanced Mechatronic Systems
Volume	3
Issue number	3
DOIs	https://doi.org/10.1504/IJAMECHS.2011.042612
Publication status	Published - 2011

Keywords

Adaptive control
Combined control
Dive overhead attack technology
Fuzzy control
Reaction-jet control

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10.1504/IJAMECHS.2011.042612

Cite this

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abstract = "In this paper, combined attitude control of the terminal trajectory for an aerial vehicle is presented. The combined attitude controller includes the fuzzy adaptive aerodynamic force mode control and the direct lateral thrust mode control. The dynamic and kinematics mathematical models of the aerial vehicle are built based on the designed reaction-jet control scheme. Simulation results show that the combined control system can satisfy the requirements of the aerial vehicle overload better than the traditional mode does.",

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AU - Fan, Ning Jun

AU - Lu, Jing

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N2 - In this paper, combined attitude control of the terminal trajectory for an aerial vehicle is presented. The combined attitude controller includes the fuzzy adaptive aerodynamic force mode control and the direct lateral thrust mode control. The dynamic and kinematics mathematical models of the aerial vehicle are built based on the designed reaction-jet control scheme. Simulation results show that the combined control system can satisfy the requirements of the aerial vehicle overload better than the traditional mode does.

AB - In this paper, combined attitude control of the terminal trajectory for an aerial vehicle is presented. The combined attitude controller includes the fuzzy adaptive aerodynamic force mode control and the direct lateral thrust mode control. The dynamic and kinematics mathematical models of the aerial vehicle are built based on the designed reaction-jet control scheme. Simulation results show that the combined control system can satisfy the requirements of the aerial vehicle overload better than the traditional mode does.

KW - Adaptive control

KW - Combined control

KW - Dive overhead attack technology

KW - Fuzzy control

KW - Reaction-jet control

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JO - International Journal of Advanced Mechatronic Systems

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IS - 3

ER -

Modelling and simulation of an aerial vehicle steering to hit on top of the target at terminal trajectory

Abstract

Keywords

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