Two controller designs of hypersonic flight vehicle under actuator dynamics and AOA constraint

Yuyan Guo; Bin Xu; Xiaoxiang Hu; Xiangwei Bu; Yu Zhang

doi:10.1016/j.ast.2018.06.025

Two controller designs of hypersonic flight vehicle under actuator dynamics and AOA constraint

Yuyan Guo, Bin Xu, Xiaoxiang Hu, Xiangwei Bu, Yu Zhang

School of Automation

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

26 Scopus citations

Abstract

This paper studies the controller design for hypersonic flight vehicle (HFV) considering the actuator hysteresis and the angle of attack (AOA) constraint respectively. Firstly, the effect of input hysteresis dynamics are regarded as the combination of the partial loss of effectiveness (PLOE) and a bounded disturbance-like item, while the controller is modified by constructing adaptive compensation laws. Secondly, to ensure the constraint on AOA, a prescribed performance control (PPC) method is designed while the AOA tracking error is restricted by the pre-defined performance function. The two controllers are designed based on dynamic surface control, where a nonlinear adaptive filter is utilized to eliminate the bound layer error. The effectiveness of the designed controllers are demonstrated via the simulation results.

Original language	English
Pages (from-to)	11-19
Number of pages	9
Journal	Aerospace Science and Technology
Volume	80
DOIs	https://doi.org/10.1016/j.ast.2018.06.025
State	Published - Sep 2018

Keywords

Adaptive control
AOA constraint
Dynamic surface control
Hypersonic flight vehicle
Input hysteresis
Prescribed performance control

Access to Document

10.1016/j.ast.2018.06.025

Cite this

@article{b5a0c1f20ea04400b62ae556e4415eae,

title = "Two controller designs of hypersonic flight vehicle under actuator dynamics and AOA constraint",

abstract = "This paper studies the controller design for hypersonic flight vehicle (HFV) considering the actuator hysteresis and the angle of attack (AOA) constraint respectively. Firstly, the effect of input hysteresis dynamics are regarded as the combination of the partial loss of effectiveness (PLOE) and a bounded disturbance-like item, while the controller is modified by constructing adaptive compensation laws. Secondly, to ensure the constraint on AOA, a prescribed performance control (PPC) method is designed while the AOA tracking error is restricted by the pre-defined performance function. The two controllers are designed based on dynamic surface control, where a nonlinear adaptive filter is utilized to eliminate the bound layer error. The effectiveness of the designed controllers are demonstrated via the simulation results.",

keywords = "Adaptive control, AOA constraint, Dynamic surface control, Hypersonic flight vehicle, Input hysteresis, Prescribed performance control",

author = "Yuyan Guo and Bin Xu and Xiaoxiang Hu and Xiangwei Bu and Yu Zhang",

note = "Publisher Copyright: {\textcopyright} 2018 Elsevier Masson SAS",

year = "2018",

month = sep,

doi = "10.1016/j.ast.2018.06.025",

language = "英语",

volume = "80",

pages = "11--19",

journal = "Aerospace Science and Technology",

issn = "1270-9638",

publisher = "Elsevier Masson s.r.l.",

}

TY - JOUR

T1 - Two controller designs of hypersonic flight vehicle under actuator dynamics and AOA constraint

AU - Guo, Yuyan

AU - Xu, Bin

AU - Hu, Xiaoxiang

AU - Bu, Xiangwei

AU - Zhang, Yu

PY - 2018/9

Y1 - 2018/9

N2 - This paper studies the controller design for hypersonic flight vehicle (HFV) considering the actuator hysteresis and the angle of attack (AOA) constraint respectively. Firstly, the effect of input hysteresis dynamics are regarded as the combination of the partial loss of effectiveness (PLOE) and a bounded disturbance-like item, while the controller is modified by constructing adaptive compensation laws. Secondly, to ensure the constraint on AOA, a prescribed performance control (PPC) method is designed while the AOA tracking error is restricted by the pre-defined performance function. The two controllers are designed based on dynamic surface control, where a nonlinear adaptive filter is utilized to eliminate the bound layer error. The effectiveness of the designed controllers are demonstrated via the simulation results.

AB - This paper studies the controller design for hypersonic flight vehicle (HFV) considering the actuator hysteresis and the angle of attack (AOA) constraint respectively. Firstly, the effect of input hysteresis dynamics are regarded as the combination of the partial loss of effectiveness (PLOE) and a bounded disturbance-like item, while the controller is modified by constructing adaptive compensation laws. Secondly, to ensure the constraint on AOA, a prescribed performance control (PPC) method is designed while the AOA tracking error is restricted by the pre-defined performance function. The two controllers are designed based on dynamic surface control, where a nonlinear adaptive filter is utilized to eliminate the bound layer error. The effectiveness of the designed controllers are demonstrated via the simulation results.

KW - Adaptive control

KW - AOA constraint

KW - Dynamic surface control

KW - Hypersonic flight vehicle

KW - Input hysteresis

KW - Prescribed performance control

UR - http://www.scopus.com/inward/record.url?scp=85049741563&partnerID=8YFLogxK

U2 - 10.1016/j.ast.2018.06.025

DO - 10.1016/j.ast.2018.06.025

M3 - 文章

AN - SCOPUS:85049741563

SN - 1270-9638

VL - 80

SP - 11

EP - 19

JO - Aerospace Science and Technology

JF - Aerospace Science and Technology

ER -

Two controller designs of hypersonic flight vehicle under actuator dynamics and AOA constraint

Abstract

Keywords

Access to Document

Other files and links

Fingerprint

Cite this