Adaptive variable structure guidance law considering missile's dynamics of autopilot

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

25 Scopus citations

Original language	English
Pages (from-to)	245
Number of pages	1
Journal	Yuhang Xuebao/Journal of Astronautics
Volume	24
Issue number	3
State	Published - May 2003

Cite this

@article{f82b80eacc774f958f5b70d190f82369,

title = "Adaptive variable structure guidance law considering missile's dynamics of autopilot",

author = "She, \{Wen Xue\} and Jun Zhou and Zhou, \{Feng Qi\}",

year = "2003",

month = may,

language = "英语",

volume = "24",

pages = "245",

journal = "Yuhang Xuebao/Journal of Astronautics",

issn = "1000-1328",

publisher = "Chinese Society of Astronautics",

number = "3",

}

TY - JOUR

T1 - Adaptive variable structure guidance law considering missile's dynamics of autopilot

AU - She, Wen Xue

AU - Zhou, Jun

AU - Zhou, Feng Qi

PY - 2003/5

Y1 - 2003/5

UR - https://www.scopus.com/pages/publications/0141817871

M3 - 文章

AN - SCOPUS:0141817871

SN - 1000-1328

VL - 24

SP - 245

JO - Yuhang Xuebao/Journal of Astronautics

JF - Yuhang Xuebao/Journal of Astronautics

IS - 3

ER -