Simplified longitudinal control of air-breathing hypersonic vehicles with hybrid actuators

Hao An; Qianqian Wu; Guan Wang; Ziyi Guo; Changhong Wang

doi:10.1016/j.ast.2020.105936

Simplified longitudinal control of air-breathing hypersonic vehicles with hybrid actuators

Hao An^*
, Qianqian Wu
, Guan Wang
, Ziyi Guo
, Changhong Wang

^*Corresponding author for this work

School of Astronautics

Harbin Institute of Technology

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

19 Scopus citations

Abstract

This paper considers the longitudinal compound control of air-breathing hypersonic vehicles configured with hybrid aerodynamic control surface (ACS) and reaction control system (RCS). In the altitude loop, the proposed nonadaptive back-stepping design results in a simplified ACS-RCS compound control. This is attributable to the introduced tangent tracking errors and ACS-RCS fusion algorithm. ACS nonlinearity, RCS quantization, and modeling parametric uncertainties are handled. In the velocity loop, the performance guaranteed adaptive control is enhanced with the bound estimation mechanism, which accommodates modeling parametric uncertainties with a low dynamic order. The effectiveness of the proposed control is verified via simulations.

Original language	English
Article number	105936
Journal	Aerospace Science and Technology
Volume	104
DOIs	https://doi.org/10.1016/j.ast.2020.105936
State	Published - Sep 2020

Keywords

Hybrid actuators
Hypersonic vehicle
Longitudinal control
Simplified algorithm

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10.1016/j.ast.2020.105936

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title = "Simplified longitudinal control of air-breathing hypersonic vehicles with hybrid actuators",

abstract = "This paper considers the longitudinal compound control of air-breathing hypersonic vehicles configured with hybrid aerodynamic control surface (ACS) and reaction control system (RCS). In the altitude loop, the proposed nonadaptive back-stepping design results in a simplified ACS-RCS compound control. This is attributable to the introduced tangent tracking errors and ACS-RCS fusion algorithm. ACS nonlinearity, RCS quantization, and modeling parametric uncertainties are handled. In the velocity loop, the performance guaranteed adaptive control is enhanced with the bound estimation mechanism, which accommodates modeling parametric uncertainties with a low dynamic order. The effectiveness of the proposed control is verified via simulations.",

keywords = "Hybrid actuators, Hypersonic vehicle, Longitudinal control, Simplified algorithm",

author = "Hao An and Qianqian Wu and Guan Wang and Ziyi Guo and Changhong Wang",

note = "Publisher Copyright: {\textcopyright} 2020 Elsevier Masson SAS",

year = "2020",

month = sep,

doi = "10.1016/j.ast.2020.105936",

language = "英语",

volume = "104",

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T1 - Simplified longitudinal control of air-breathing hypersonic vehicles with hybrid actuators

AU - An, Hao

AU - Wu, Qianqian

AU - Wang, Guan

AU - Guo, Ziyi

AU - Wang, Changhong

PY - 2020/9

Y1 - 2020/9

N2 - This paper considers the longitudinal compound control of air-breathing hypersonic vehicles configured with hybrid aerodynamic control surface (ACS) and reaction control system (RCS). In the altitude loop, the proposed nonadaptive back-stepping design results in a simplified ACS-RCS compound control. This is attributable to the introduced tangent tracking errors and ACS-RCS fusion algorithm. ACS nonlinearity, RCS quantization, and modeling parametric uncertainties are handled. In the velocity loop, the performance guaranteed adaptive control is enhanced with the bound estimation mechanism, which accommodates modeling parametric uncertainties with a low dynamic order. The effectiveness of the proposed control is verified via simulations.

AB - This paper considers the longitudinal compound control of air-breathing hypersonic vehicles configured with hybrid aerodynamic control surface (ACS) and reaction control system (RCS). In the altitude loop, the proposed nonadaptive back-stepping design results in a simplified ACS-RCS compound control. This is attributable to the introduced tangent tracking errors and ACS-RCS fusion algorithm. ACS nonlinearity, RCS quantization, and modeling parametric uncertainties are handled. In the velocity loop, the performance guaranteed adaptive control is enhanced with the bound estimation mechanism, which accommodates modeling parametric uncertainties with a low dynamic order. The effectiveness of the proposed control is verified via simulations.

KW - Hybrid actuators

KW - Hypersonic vehicle

KW - Longitudinal control

KW - Simplified algorithm

UR - https://www.scopus.com/pages/publications/85086501556

U2 - 10.1016/j.ast.2020.105936

DO - 10.1016/j.ast.2020.105936

M3 - 文章

AN - SCOPUS:85086501556

SN - 1270-9638

VL - 104

JO - Aerospace Science and Technology

JF - Aerospace Science and Technology

M1 - 105936

ER -

Simplified longitudinal control of air-breathing hypersonic vehicles with hybrid actuators

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Keywords

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