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

Uçak Mühendisliği Bölümü

Samara State Technical University
Samara National Research University

Araştırma sonucu: Dergiye katkı › Konferans makalesi › bilirkişi

4 Atıf (Scopus)

Özet

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.

Orijinal dil	İngilizce
Sayfa (başlangıç-bitiş)	222-227
Sayfa sayısı	6
Dergi	IFAC-PapersOnLine
Hacim	28
Basın numarası	9
DOI'lar	https://doi.org/10.1016/j.ifacol.2015.08.087
Yayın durumu	Yayınlandı - 1 Tem 2015
Etkinlik	1st IFAC Workshop on Advanced Control and Navigation for Autonomous Aerospace Vehicles, ACNAAV 2015 - Seville, Spain Süre: 10 Haz 2015 → 12 Haz 2015

Bibliyografik not

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

Finansman

★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)

Finansörler	Finansör numarası
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

Belgeye Erişim

10.1016/j.ifacol.2015.08.087

Diğer Dosyalar ve Linkler

Link to publication in Scopus

Alıntı Yap

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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",

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

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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

Özet

Bibliyografik not

Finansman

Belgeye Erişim

Diğer Dosyalar ve Linkler

Parmak izi

Alıntı Yap