Research on spin rocket double-channel proportional control characteristics

Bo Mo; En Yu Gao; Shu Xing Yang

doi:10.1109/ICICIC.2007.486

Research on spin rocket double-channel proportional control characteristics

Bo Mo^*, En Yu Gao, Shu Xing Yang

^*Corresponding author for this work

School of Aerospace Engineering

Beijing Institute of Technology

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

4 Citations (Scopus)

Abstract

This paper mainly focuses on double-channel proportional control characteristic of the endoatmospheric spin rocket. The divided command model is built under spin condition and the control process is simulated in mathematic method. In the end, it is conclusion of spin rocket proportional control characteristic.

Original language	English
Title of host publication	Second International Conference on Innovative Computing, Information and Control, ICICIC 2007
Publisher	IEEE Computer Society
ISBN (Print)	0769528821, 9780769528823
DOIs	https://doi.org/10.1109/ICICIC.2007.486
Publication status	Published - 2007
Event	2nd International Conference on Innovative Computing, Information and Control, ICICIC 2007 - Kumamoto, Japan Duration: 5 Sept 2007 → 7 Sept 2007

Publication series

Name	Second International Conference on Innovative Computing, Information and Control, ICICIC 2007

Conference

Conference	2nd International Conference on Innovative Computing, Information and Control, ICICIC 2007
Country/Territory	Japan
City	Kumamoto
Period	5/09/07 → 7/09/07

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10.1109/ICICIC.2007.486

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Mo, B., Gao, E. Y., & Yang, S. X. (2007). Research on spin rocket double-channel proportional control characteristics. In Second International Conference on Innovative Computing, Information and Control, ICICIC 2007 Article 4427659 (Second International Conference on Innovative Computing, Information and Control, ICICIC 2007). IEEE Computer Society. https://doi.org/10.1109/ICICIC.2007.486

@inproceedings{e1ad88cc352441488bbae1632eaa7fc4,

title = "Research on spin rocket double-channel proportional control characteristics",

abstract = "This paper mainly focuses on double-channel proportional control characteristic of the endoatmospheric spin rocket. The divided command model is built under spin condition and the control process is simulated in mathematic method. In the end, it is conclusion of spin rocket proportional control characteristic.",

author = "Bo Mo and Gao, {En Yu} and Yang, {Shu Xing}",

year = "2007",

doi = "10.1109/ICICIC.2007.486",

language = "English",

isbn = "0769528821",

series = "Second International Conference on Innovative Computing, Information and Control, ICICIC 2007",

publisher = "IEEE Computer Society",

booktitle = "Second International Conference on Innovative Computing, Information and Control, ICICIC 2007",

address = "United States",

note = "2nd International Conference on Innovative Computing, Information and Control, ICICIC 2007 ; Conference date: 05-09-2007 Through 07-09-2007",

}

Mo, B, Gao, EY & Yang, SX 2007, Research on spin rocket double-channel proportional control characteristics. in Second International Conference on Innovative Computing, Information and Control, ICICIC 2007., 4427659, Second International Conference on Innovative Computing, Information and Control, ICICIC 2007, IEEE Computer Society, 2nd International Conference on Innovative Computing, Information and Control, ICICIC 2007, Kumamoto, Japan, 5/09/07. https://doi.org/10.1109/ICICIC.2007.486

Research on spin rocket double-channel proportional control characteristics. / Mo, Bo; Gao, En Yu; Yang, Shu Xing.
Second International Conference on Innovative Computing, Information and Control, ICICIC 2007. IEEE Computer Society, 2007. 4427659 (Second International Conference on Innovative Computing, Information and Control, ICICIC 2007).

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

TY - GEN

T1 - Research on spin rocket double-channel proportional control characteristics

AU - Mo, Bo

AU - Gao, En Yu

AU - Yang, Shu Xing

PY - 2007

Y1 - 2007

N2 - This paper mainly focuses on double-channel proportional control characteristic of the endoatmospheric spin rocket. The divided command model is built under spin condition and the control process is simulated in mathematic method. In the end, it is conclusion of spin rocket proportional control characteristic.

AB - This paper mainly focuses on double-channel proportional control characteristic of the endoatmospheric spin rocket. The divided command model is built under spin condition and the control process is simulated in mathematic method. In the end, it is conclusion of spin rocket proportional control characteristic.

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U2 - 10.1109/ICICIC.2007.486

DO - 10.1109/ICICIC.2007.486

M3 - Conference contribution

AN - SCOPUS:39049095711

SN - 0769528821

SN - 9780769528823

T3 - Second International Conference on Innovative Computing, Information and Control, ICICIC 2007

BT - Second International Conference on Innovative Computing, Information and Control, ICICIC 2007

PB - IEEE Computer Society

T2 - 2nd International Conference on Innovative Computing, Information and Control, ICICIC 2007

Y2 - 5 September 2007 through 7 September 2007

ER -

Research on spin rocket double-channel proportional control characteristics

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