面向飞推一体化的飞行器建模方法

Xue Kong; Guodong Ning; Ming Yang; Songyan Wang; Tao Chao

doi:10.3969/j.issn.1001-506X.2019.01.20

面向飞推一体化的飞行器建模方法

Translated title of the contribution: Modeling method oriented to vehicle of integrated flight/propulsion

Xue Kong
, Guodong Ning
, Ming Yang
, Songyan Wang
, Tao Chao

School of Astronautics

Harbin Institute of Technology
CAS - Institute of Mechanics

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

1 Scopus citations

Abstract

The airbreathing hypersonic vehicle (ABHV) is a typical vehicle which has multidimensional nonlinear restrictions and intricate coupling. Due to the strong coupling interactions and multidimensional nonlinear restrictionists, the flight powered by scramjet is a critical phase of reference trajectory, guidance and control designing. Therefore, the development of a reasonable ABHV model is inevitable. The existing models of integrated aircraft-scramjet are difficult for control design directly, and also can not be used with a numeric model together. To achieve the goal of exhuming the potential applications and expanding flight feasibility of ABHV, and improving the efficiency and robustness of ABHV from the overall level, based on the working mechanism and numerical model of scramjet, the performance and protected model of scramjet is researched, and the control oriented model of ABHV is developed.

Translated title of the contribution	Modeling method oriented to vehicle of integrated flight/propulsion
Original language	Chinese (Traditional)
Pages (from-to)	141-147
Number of pages	7
Journal	Xi Tong Gong Cheng Yu Dian Zi Ji Shu/Systems Engineering and Electronics
Volume	41
Issue number	1
DOIs	https://doi.org/10.3969/j.issn.1001-506X.2019.01.20
State	Published - 1 Jan 2019

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10.3969/j.issn.1001-506X.2019.01.20

Cite this

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title = "面向飞推一体化的飞行器建模方法",

abstract = "The airbreathing hypersonic vehicle (ABHV) is a typical vehicle which has multidimensional nonlinear restrictions and intricate coupling. Due to the strong coupling interactions and multidimensional nonlinear restrictionists, the flight powered by scramjet is a critical phase of reference trajectory, guidance and control designing. Therefore, the development of a reasonable ABHV model is inevitable. The existing models of integrated aircraft-scramjet are difficult for control design directly, and also can not be used with a numeric model together. To achieve the goal of exhuming the potential applications and expanding flight feasibility of ABHV, and improving the efficiency and robustness of ABHV from the overall level, based on the working mechanism and numerical model of scramjet, the performance and protected model of scramjet is researched, and the control oriented model of ABHV is developed.",

keywords = "Control-oriented modeling, Integrated flight/propulsion, Multidimensional nonlinear restriction, Strong coupling interaction",

author = "Xue Kong and Guodong Ning and Ming Yang and Songyan Wang and Tao Chao",

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T1 - 面向飞推一体化的飞行器建模方法

AU - Kong, Xue

AU - Ning, Guodong

AU - Yang, Ming

AU - Wang, Songyan

AU - Chao, Tao

PY - 2019/1/1

Y1 - 2019/1/1

N2 - The airbreathing hypersonic vehicle (ABHV) is a typical vehicle which has multidimensional nonlinear restrictions and intricate coupling. Due to the strong coupling interactions and multidimensional nonlinear restrictionists, the flight powered by scramjet is a critical phase of reference trajectory, guidance and control designing. Therefore, the development of a reasonable ABHV model is inevitable. The existing models of integrated aircraft-scramjet are difficult for control design directly, and also can not be used with a numeric model together. To achieve the goal of exhuming the potential applications and expanding flight feasibility of ABHV, and improving the efficiency and robustness of ABHV from the overall level, based on the working mechanism and numerical model of scramjet, the performance and protected model of scramjet is researched, and the control oriented model of ABHV is developed.

AB - The airbreathing hypersonic vehicle (ABHV) is a typical vehicle which has multidimensional nonlinear restrictions and intricate coupling. Due to the strong coupling interactions and multidimensional nonlinear restrictionists, the flight powered by scramjet is a critical phase of reference trajectory, guidance and control designing. Therefore, the development of a reasonable ABHV model is inevitable. The existing models of integrated aircraft-scramjet are difficult for control design directly, and also can not be used with a numeric model together. To achieve the goal of exhuming the potential applications and expanding flight feasibility of ABHV, and improving the efficiency and robustness of ABHV from the overall level, based on the working mechanism and numerical model of scramjet, the performance and protected model of scramjet is researched, and the control oriented model of ABHV is developed.

KW - Control-oriented modeling

KW - Integrated flight/propulsion

KW - Multidimensional nonlinear restriction

KW - Strong coupling interaction

UR - https://www.scopus.com/pages/publications/85063365693

U2 - 10.3969/j.issn.1001-506X.2019.01.20

DO - 10.3969/j.issn.1001-506X.2019.01.20

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JO - Xi Tong Gong Cheng Yu Dian Zi Ji Shu/Systems Engineering and Electronics

JF - Xi Tong Gong Cheng Yu Dian Zi Ji Shu/Systems Engineering and Electronics

IS - 1

ER -

面向飞推一体化的飞行器建模方法

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