Robust saturated finite-time attitude control for spacecraft using integral sliding mode

Yong Guo, Bing Huang, Shen Min Song, Ai Jun Li, Chang Qing Wang

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

67 Scopus citations

Original language	English
Pages (from-to)	440-446
Number of pages	7
Journal	Journal of Guidance, Control, and Dynamics
Volume	42
Issue number	2
DOIs	https://doi.org/10.2514/1.G003520
State	Published - 2019

Access to Document

@article{812a91c76c8b40c990d01a752e6e83fd,

title = "Robust saturated finite-time attitude control for spacecraft using integral sliding mode",

author = "Yong Guo and Bing Huang and Song, {Shen Min} and Li, {Ai Jun} and Wang, {Chang Qing}",

year = "2019",

doi = "10.2514/1.G003520",

language = "英语",

volume = "42",

pages = "440--446",

journal = "Journal of Guidance, Control, and Dynamics",

issn = "0731-5090",

publisher = "American Institute of Aeronautics and Astronautics Inc. (AIAA)",

number = "2",

}

TY - JOUR

T1 - Robust saturated finite-time attitude control for spacecraft using integral sliding mode

AU - Guo, Yong

AU - Huang, Bing

AU - Song, Shen Min

AU - Li, Ai Jun

AU - Wang, Chang Qing

PY - 2019

Y1 - 2019

UR - http://www.scopus.com/inward/record.url?scp=85067401152&partnerID=8YFLogxK

U2 - 10.2514/1.G003520

DO - 10.2514/1.G003520

M3 - 文章

AN - SCOPUS:85067401152

SN - 0731-5090

VL - 42

SP - 440

EP - 446

JO - Journal of Guidance, Control, and Dynamics

JF - Journal of Guidance, Control, and Dynamics

IS - 2

ER -