Attitude guidance, navigation and control of land-survey mini-satellites

Ye Somov; S. Butyrin; S. Somov; C. Hajiyev

doi:10.1016/j.ifacol.2015.08.087

Attitude guidance, navigation and control of land-survey mini-satellites

Ye Somov, S. Butyrin, S. Somov, C. Hajiyev

Department of Aeronautical Engineering

Research output: Contribution to journal › Conference article › peer-review

4 Citations (Scopus)

Abstract

Contemporary land-survey mini-satellites have general mass up to 500 kg and are placed onto the orbit altitudes up to 800 km. For such spacecraft some principle problems on optimal attitude guidance, navigation and robust control are considered and elaborated methods are presented for their solving.

Original language	English
Pages (from-to)	222-227
Number of pages	6
Journal	IFAC-PapersOnLine
Volume	28
Issue number	9
DOIs	https://doi.org/10.1016/j.ifacol.2015.08.087
Publication status	Published - 1 Jul 2015
Event	1st IFAC Workshop on Advanced Control and Navigation for Autonomous Aerospace Vehicles, ACNAAV 2015 - Seville, Spain Duration: 10 Jun 2015 → 12 Jun 2015

Bibliographical note

Publisher Copyright:
© 2015, IFAC (International Federation of Automatic Control) Hosting by Elsevier Ltd. All rights reserved.

Funding

★This work was supported by RFBR (Russian Foundation for ★This work was supported by RFBR (Russian Foundation for BaTsihcisRewseoarkrchw,aGsrasuntpp1o4r-t0e8d-91b3y73R),FTBURBI(TRAusKsia(TnhFeoSucniednattiifoicn afnodr Basic Research, Grant 14-08-91373), TUBITAK (The Scientific and TeacshicnoRloesgeicaarclhR,eGseraarncth1C4o-0u8n-c9i1l 3o7f3T)u, rTkUeyB, GITrAanKt 1(T13hEe5S9c5i)enatnidficDaivnid-Basic Research, Grant 14-08-91373), TUBITAK (The Scientific and TieocnhnonoloEgMicMalCRPe,seRaurcshsiaCnouAnccaildoemf Tyuorkf eSyc,ieGnrcaenst(1P1r3oEg5ra9m5) nano.d1D3i)vi-Technological Research Council of Turkey, Grant 113E595) and Division on EMMCP, Russian Academy of Sciences (Program no. 13)

Funders	Funder number
Division on EMMCP
FTBURBI	14-08-91373
Russian Foundation for BaTsihcisRewseoarkrchw,aGsrasuntpp1o4r-t0e8d-91b3y73R
TUBITAK	113E595, TeacshicnoRloesgeicaarclhR,eGseraarncth1C4o-0u8n-c9i1l 3o7f3T, 1P1r3oEg5ra9m5
Russian Foundation for Basic Research
Russian Academy of Sciences	13

Keywords

Attitude control
Guidance
Mini-satellite
Navigation

Access to Document

10.1016/j.ifacol.2015.08.087

Cite this

@article{b146ee2889c2496d8b1ddf0adbbbb609,

title = "Attitude guidance, navigation and control of land-survey mini-satellites",

abstract = "Contemporary land-survey mini-satellites have general mass up to 500 kg and are placed onto the orbit altitudes up to 800 km. For such spacecraft some principle problems on optimal attitude guidance, navigation and robust control are considered and elaborated methods are presented for their solving.",

keywords = "Attitude control, Guidance, Mini-satellite, Navigation",

author = "Ye Somov and S. Butyrin and S. Somov and C. Hajiyev",

note = "Publisher Copyright: {\textcopyright} 2015, IFAC (International Federation of Automatic Control) Hosting by Elsevier Ltd. All rights reserved.; 1st IFAC Workshop on Advanced Control and Navigation for Autonomous Aerospace Vehicles, ACNAAV 2015 ; Conference date: 10-06-2015 Through 12-06-2015",

year = "2015",

month = jul,

day = "1",

doi = "10.1016/j.ifacol.2015.08.087",

language = "English",

volume = "28",

pages = "222--227",

journal = "IFAC-PapersOnLine",

issn = "2405-8963",

publisher = "Elsevier B.V.",

number = "9",

}

TY - JOUR

T1 - Attitude guidance, navigation and control of land-survey mini-satellites

AU - Somov, Ye

AU - Butyrin, S.

AU - Somov, S.

AU - Hajiyev, C.

PY - 2015/7/1

Y1 - 2015/7/1

N2 - Contemporary land-survey mini-satellites have general mass up to 500 kg and are placed onto the orbit altitudes up to 800 km. For such spacecraft some principle problems on optimal attitude guidance, navigation and robust control are considered and elaborated methods are presented for their solving.

AB - Contemporary land-survey mini-satellites have general mass up to 500 kg and are placed onto the orbit altitudes up to 800 km. For such spacecraft some principle problems on optimal attitude guidance, navigation and robust control are considered and elaborated methods are presented for their solving.

KW - Attitude control

KW - Guidance

KW - Mini-satellite

KW - Navigation

UR - https://www.scopus.com/pages/publications/84992482491

U2 - 10.1016/j.ifacol.2015.08.087

DO - 10.1016/j.ifacol.2015.08.087

M3 - Conference article

AN - SCOPUS:84992482491

SN - 2405-8963

VL - 28

SP - 222

EP - 227

JO - IFAC-PapersOnLine

JF - IFAC-PapersOnLine

IS - 9

T2 - 1st IFAC Workshop on Advanced Control and Navigation for Autonomous Aerospace Vehicles, ACNAAV 2015

Y2 - 10 June 2015 through 12 June 2015

ER -

Attitude guidance, navigation and control of land-survey mini-satellites

Abstract

Bibliographical note

Funding

Keywords

Access to Document

Other files and links

Fingerprint

Cite this