STANDALONE THREE-AXIS ATTITUDE DETERMINATION FROM EARTH IMAGES

被引：0

作者：

Bevilacqua, A. ^{[1
]}

Bianchi, C. ^{[2
]}

Carozza, L. ^{[3
]}

Gherardi, A. ^{[3
]}

Melega, N. ^{[4
]}

Modenini, D. ^{[4
]}

Tortora, P. ^{[4
]}

机构：

[1] Univ Bologna, DEIS, Viale Risorgimento 2, I-40136 Bologna, Italy

[2] ALMASpace Srl, Opt Syst, I-47121 Forli, FC, Italy

[3] Univ Bologna, ARCES, I-40125 Bologna, Italy

[4] Univ Bologna, DIEM, I-47121 Forli, FC, Italy

来源：

SPACEFLIGHT MECHANICS 2010, PTS I-III | 2010年 / 136卷

关键词：

D O I：

暂无

中图分类号：

TP [自动化技术、计算机技术];

学科分类号：

0812 ;

摘要：

The feasibility of a novel standalone spacecraft attitude sensor, capable of estimating the full three axis orientation of an Earth-orbiting satellite is investigated in this paper. The underlying idea is that by capturing from space a sequence of images of the Earth surface (in the visible bands) and elaborating them in pairs, S/C attitude could be reconstructed. The following project steps were followed in about two years and are thoroughly discussed in the paper: selection of enabling technologies, definition of the attitude determination algorithm, numerical simulations followed by an acquisition campaign on a experimental test-bed.

引用

页码：695 / +

页数：2

共 50 条

[1] Three-axis attitude propagation from digital images
Lopes, RVF
Silva, AR
Kuga, HK
MALCOLM D. SHUSTER ASTRONAUTICS SYMPOSIUM, 2006, 122 : 289 - +
[2] Deterministic Three-Axis Attitude Determination
Sinister, Malcolm D.
Journal of the Astronautical Sciences, 2004, 52 (03): : 405 - 419
[3] Three-axis magnetometer attitude determination
Tian, Jing
Wu, Mei-Ping
Hu, Xiao-Ping
Guofang Keji Daxue Xuebao/Journal of National University of Defense Technology, 2001, 23 (05):
[4] Three-Axis Attitude Determination Using Magnetorquers
Ivanov, Danil
Ovchinnikov, Mikhail
Roldugin, Dmitry
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2018, 41 (11) : 2455 - 2462
[5] Three-Axis Sun Sensor for Attitude Determination
Liebe, Carl C.
Murphy, Neil
Dorsky, Len
Udomkesmalee, Nythi
IEEE AEROSPACE AND ELECTRONIC SYSTEMS MAGAZINE, 2016, 31 (06) : 6 - 11
[6] Three-axis attitude determination from incomplete two vector observations
Tan C.
Gao X.
Xu G.
Chen S.
Yi Qi Yi Biao Xue Bao/Chinese Journal of Scientific Instrument, 2018, 39 (11): : 140 - 146
[7] Spacecraft attitude determination and three-axis magnetometer calibration
Huang, Lin
Jing, Wu-Xing
Yuhang Xuebao/Journal of Astronautics, 2008, 29 (03): : 854 - 859
[8] Three-axis attitude determination using incomplete vector observations
Lee, Seon-Ho
Ahn, Hyo-Sung
Yong, Ki-Lyuk
ACTA ASTRONAUTICA, 2009, 65 (7-8) : 1089 - 1093
[9] Attitude determination using combined GPS and three-axis magnetometer data
Crassidis, J.L., 2001, Lister Science (20):
[10] Three-Axis Attitude Determination of a Nanosatellite Using Optimized TRIAD Algorithms
Kirci, Orhan
Hajiyev, Chingiz
INFORMATION TECHNOLOGIES AND THEIR APPLICATIONS, PT II, ITTA 2024, 2025, 2226 : 159 - 170

← 1 2 3 4 5 →