Nanosatellite reflector for optical calibrations: Attitude control and determination aspects

被引：3
|
作者：
Shargorodsky, V
Shevchenko, V
Ovchinnikov, M
Penkov, V
Mirer, S
Nemuchinsky, R
机构：
[1] SRIPDE SDEC, Moscow 111250, Russia
[2] RAS, KIAM, Moscow 125047, Russia
[3] Moscow Phys Tech Inst, Dolgoprudnyi 141700, Moscow Region, Russia
来源：
NEW TRENDS IN SPACE GEODESY | 2002年 / 30卷 / 02期
基金：
俄罗斯基础研究基金会;
关键词：
D O I：
10.1016/S0273-1177(02)00304-6
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
Nanosatellite REFLECTOR has been designed to provide an orbital reference target for collaborative optical sensing, imaging, and tracking experiments with space objects. The satellite hosts well-calibrated laser reflectors that provide a unique target for experiments involving laser illumination. A passive gravity-gradient attitude control system is used to ensure a given angular motion of the satellite. A problem of attitude control system development and ideas of attitude determination without on-board sensors are discussed. (C) 2002 COSPAR. Published by Elsevier Science Ltd. All rights reserved.
引用
收藏
页码：337 / 343
页数：7
相关论文
共 50 条
  • [1] Nanosatellite REFLECTOR:: Choice of parameters of the attitude control system
    Ovchinnikov, M. Yu.
    Shargorodskiy, V. D.
    Pen'kov, V. I.
    Mirer, S. A.
    Guerman, A. D.
    Nemuchinskiy, R. B.
    COSMIC RESEARCH, 2007, 45 (01) : 60 - 77
  • [2] Nanosatellite REFLECTOR: Choice of parameters of the attitude control system
    M. Yu. Ovchinnikov
    V. D. Shargorodskiy
    V. I. Pen’kov
    S. A. Mirer
    A. D. Guerman
    R. B. Nemuchinskiy
    Cosmic Research, 2007, 45 : 60 - 77
  • [3] Design and implementation of a nanosatellite attitude determination and control system
    Makovec, KL
    Turner, AJ
    Hall, CD
    ASTRODYNAMICS 2001, PTS I-III, 2001, 109 : 167 - 185
  • [4] Design of Attitude Determination and Control System using Microstrip Magnetorquer for Nanosatellite
    Haryadi, Defrandi Renanda
    Wijanto, Heroe
    Syihabuddin, Budi
    Prasetyo, Agus D.
    2016 INTERNATIONAL CONFERENCE ON CONTROL, ELECTRONICS, RENEWABLE ENERGY AND COMMUNICATIONS (ICCEREC), 2016, : 65 - 69
  • [5] Design and Verification of the Operating Procedure of Attitude Determination and Control Subsystem of a Nanosatellite
    Lin, Ting-Yang
    Juang, Jyh-Ching
    Vina
    2014 CACS INTERNATIONAL AUTOMATIC CONTROL CONFERENCE (CACS 2014), 2014, : 51 - 56
  • [6] Attitude determination and control for centrifugal tether deployment on the ESTCube-1 nanosatellite
    Slavinskis, Andris
    Kulu, Erik
    Viru, Jaan
    Valner, Robert
    Ehrpais, Hendrik
    Uiboupin, Tonis
    Jaerve, Markus
    Soolo, Endel
    Envall, Jouni
    Scheffler, Tobias
    Suenter, Indrek
    Kuuste, Henri
    Kvell, Urmas
    Kalde, Jaanus
    Laizans, Kaspars
    Ilbis, Erik
    Eenmaee, Tonis
    Vendt, Riho
    Voormansik, Kaupo
    Ansko, Ilmar
    Allik, Viljo
    Laett, Silver
    Noorma, Mart
    PROCEEDINGS OF THE ESTONIAN ACADEMY OF SCIENCES, 2014, 63 (02) : 242 - 249
  • [7] Fault-Tolerant Attitude Determination and Control System Design of Nanosatellite 2
    Shi, Shuai
    Yuan, Binwen
    Zhao, Kaichun
    You, Zheng
    Zhang, Gaofei
    JOURNAL OF AEROSPACE ENGINEERING, 2018, 31 (06)
  • [8] Attitude determination and control of a nanosatellite using geomagnetic field data and sun sensors
    Hur, PS
    Melton, RG
    Spencer, DB
    Spaceflight Mechanics 2004, Vol 119, Pt 1-3, 2005, 119 : 639 - 658
  • [9] A High Precision Attitude Determination and Control System for the UYS-1 Nanosatellite
    Chaurais, Jefferson R.
    Ferreira, Henrique C.
    Ishihara, Joao Y.
    Borges, Renato A.
    Kulabukhov, Anatoliy M.
    Larin, Vladimir A.
    Belikov, Vladimir V.
    2013 IEEE AEROSPACE CONFERENCE, 2013,
  • [10] Development of an Air-Bearing Testbed for Nanosatellite Attitude Determination and Control Systems
    Yanyachi, Pablo Raul
    Mamani-Saico, Alfredo
    Wang, Xinsheng
    Espinoza-Garcia, Brayan
    IEEE ACCESS, 2024, 12 : 168864 - 168876
12345