Active disturbance rejection control for drag tracking in mars entry guidance

Yuanqing Xia; Rongfang Chen; Fan Pu; Li Dai

doi:10.1016/j.asr.2013.12.008

Active disturbance rejection control for drag tracking in mars entry guidance

Yuanqing Xia^*
, Rongfang Chen
, Fan Pu
, Li Dai

^*此作品的通讯作者

自动化学院

Beijing Institute of Technology

科研成果: 期刊稿件 › 文章 › 同行评审

91 引用（Scopus）

摘要

Future Mars missions will require precision landing capability, which motivates the need for entry closed-loop guidance schemes. A new tracking law - active disturbance rejection control (ADRC) - is presented in this paper. The ability of the ADRC tracking law to handle the atmospheric models and the vehicle's aerodynamic errors is investigated. Monte Carlo simulations with dispersions in entry state variables, drag and lift coefficients, and atmospheric density show effectiveness of the proposed algorithm.

源语言	英语
页（从-至）	853-861
页数	9
期刊	Advances in Space Research
卷	53
期	5
DOI	https://doi.org/10.1016/j.asr.2013.12.008
出版状态	已出版 - 1 3月 2014

访问文件

10.1016/j.asr.2013.12.008

其它文件与链接

链接到 Scopus 的出版物

引用此

@article{b7010967d0b748afb8a7b59d4b90ea00,

title = "Active disturbance rejection control for drag tracking in mars entry guidance",

abstract = "Future Mars missions will require precision landing capability, which motivates the need for entry closed-loop guidance schemes. A new tracking law - active disturbance rejection control (ADRC) - is presented in this paper. The ability of the ADRC tracking law to handle the atmospheric models and the vehicle's aerodynamic errors is investigated. Monte Carlo simulations with dispersions in entry state variables, drag and lift coefficients, and atmospheric density show effectiveness of the proposed algorithm.",

keywords = "ADRC, Closed-loop guidance schemes, Monte Carlo, Precision landing capability",

author = "Yuanqing Xia and Rongfang Chen and Fan Pu and Li Dai",

year = "2014",

month = mar,

day = "1",

doi = "10.1016/j.asr.2013.12.008",

language = "English",

volume = "53",

pages = "853--861",

journal = "Advances in Space Research",

issn = "0273-1177",

publisher = "Elsevier Ltd.",

number = "5",

}

TY - JOUR

T1 - Active disturbance rejection control for drag tracking in mars entry guidance

AU - Xia, Yuanqing

AU - Chen, Rongfang

AU - Pu, Fan

AU - Dai, Li

PY - 2014/3/1

Y1 - 2014/3/1

N2 - Future Mars missions will require precision landing capability, which motivates the need for entry closed-loop guidance schemes. A new tracking law - active disturbance rejection control (ADRC) - is presented in this paper. The ability of the ADRC tracking law to handle the atmospheric models and the vehicle's aerodynamic errors is investigated. Monte Carlo simulations with dispersions in entry state variables, drag and lift coefficients, and atmospheric density show effectiveness of the proposed algorithm.

AB - Future Mars missions will require precision landing capability, which motivates the need for entry closed-loop guidance schemes. A new tracking law - active disturbance rejection control (ADRC) - is presented in this paper. The ability of the ADRC tracking law to handle the atmospheric models and the vehicle's aerodynamic errors is investigated. Monte Carlo simulations with dispersions in entry state variables, drag and lift coefficients, and atmospheric density show effectiveness of the proposed algorithm.

KW - ADRC

KW - Closed-loop guidance schemes

KW - Monte Carlo

KW - Precision landing capability

UR - https://www.scopus.com/pages/publications/84893909481

U2 - 10.1016/j.asr.2013.12.008

DO - 10.1016/j.asr.2013.12.008

M3 - Article

AN - SCOPUS:84893909481

SN - 0273-1177

VL - 53

SP - 853

EP - 861

JO - Advances in Space Research

JF - Advances in Space Research

IS - 5

ER -

Active disturbance rejection control for drag tracking in mars entry guidance

摘要

访问文件

其它文件与链接

指纹

引用此