Gyroless attitude estimation of sun-pointing satellites using magnetometers

被引：15

作者：

Ahn, HS ^{[1
]}

Lee, SH

机构：

[1] Utah State Univ, Dept Elect & Comp Engn, Coll Engn, Logan, UT 84322 USA

[2] Korea Aerosp Res Inst, Satellite Control Div, Taejon, South Korea

来源：

IEEE GEOSCIENCE AND REMOTE SENSING LETTERS | 2005年 / 2卷 / 01期

关键词：

deterministic attitude estimation; magnetometer; sun-pointing satellite;

D O I：

10.1109/LGRS.2004.840608

中图分类号：

P3 [地球物理学]; P59 [地球化学];

学科分类号：

0708 ; 070902 ;

摘要：

Deterministic attitude estimation methods based on vector observations are used for the coarse-attitude calculation of the sun-pointing satellites. The objective of the deterministic attitude estimation is to get the direction cosine matrix without considering the stochastic noises. The existing deterministic attitude estimation methods require two complete (three-axis) vector observations corresponding to two known reference vectors. This letter suggests a new deterministic attitude estimation method using only geomagnetic-field measurements on two axes for sun-pointing satellites in the sun-acquisition mode.

引用

页码：8 / 12

页数：5

共 12 条

[1]

Caruso M. J., 2000, IEEE 2000. Position Location and Navigation Symposium (Cat. No.00CH37062), P177, DOI 10.1109/PLANS.2000.838300

[2]

CRASSIDIS JL, 1995, P FLIGHT MECH EST TH, P419

[3]

Crassidis John L., 2001, SPACE TECHNOLOGY, V20, P147

[4]

DEUTSCHMANN J, 1996, P AIAA AAS ASTRODYNA, P554

[5]

Gebre-Egziabher D., 2000, IEEE 2000. Position Location and Navigation Symposium (Cat. No.00CH37062), P185, DOI 10.1109/PLANS.2000.838301

[6]

Lee SH, 2004, IEEE T AERO ELEC SYS, V40, P1020

[7] A real-time kinematic GPS sensor for spacecraft relative navigation [J].

Montenbruck, O ;

Ebinuma, T ;

Lightsey, EG ;

Leung, S .

AEROSPACE SCIENCE AND TECHNOLOGY, 2002, 6 (06) :435-449

[8]

*NASA, 1996, ROS US HDB

[9] 3-AXIS ATTITUDE DETERMINATION VIA KALMAN FILTERING OF MAGNETOMETER DATA [J].

PSIAKI, ML ;

MARTEL, F ;

PAL, PK .

JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 1990, 13 (03) :506-514

[10]

Santoni F, 2000, AEROSP CONF PROC, P127, DOI 10.1109/AERO.2000.879282

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