In-Flight Identification of Magnetometer and Attitude Determination System for Land-survey Mini-satellite

Yevgeny Somov; Sergey Butyrin; Chingiz Hajiyev

doi:10.1016/j.ifacol.2015.09.153

In-Flight Identification of Magnetometer and Attitude Determination System for Land-survey Mini-satellite

Yevgeny Somov, Sergey Butyrin, Chingiz Hajiyev

Department of Aeronautical Engineering

Samara State Technical University

Research output: Contribution to journal › Article › peer-review

3 Citations (Scopus)

Abstract

We present discrete algorithms for in-flight identification, calibration and alignment of a low cost strap-down inertial navigation system with correction by signals from the Sun and magnetic sensors. Proposed algorithms are simulated through attitude dynamics of a small land-survey satellite.

Original language	English
Pages (from-to)	16-21
Number of pages	6
Journal	IFAC-PapersOnLine
Volume	48
Issue number	11 11
DOIs	https://doi.org/10.1016/j.ifacol.2015.09.153
Publication status	Published - 2015

Bibliographical note

Publisher Copyright:
© 2015

Keywords

attitude determination
calibration
identification
mini-satellite

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10.1016/j.ifacol.2015.09.153

Cite this

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title = "In-Flight Identification of Magnetometer and Attitude Determination System for Land-survey Mini-satellite",

abstract = "We present discrete algorithms for in-flight identification, calibration and alignment of a low cost strap-down inertial navigation system with correction by signals from the Sun and magnetic sensors. Proposed algorithms are simulated through attitude dynamics of a small land-survey satellite.",

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author = "Yevgeny Somov and Sergey Butyrin and Chingiz Hajiyev",

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doi = "10.1016/j.ifacol.2015.09.153",

language = "English",

volume = "48",

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T1 - In-Flight Identification of Magnetometer and Attitude Determination System for Land-survey Mini-satellite

AU - Somov, Yevgeny

AU - Butyrin, Sergey

AU - Hajiyev, Chingiz

PY - 2015

Y1 - 2015

N2 - We present discrete algorithms for in-flight identification, calibration and alignment of a low cost strap-down inertial navigation system with correction by signals from the Sun and magnetic sensors. Proposed algorithms are simulated through attitude dynamics of a small land-survey satellite.

AB - We present discrete algorithms for in-flight identification, calibration and alignment of a low cost strap-down inertial navigation system with correction by signals from the Sun and magnetic sensors. Proposed algorithms are simulated through attitude dynamics of a small land-survey satellite.

KW - attitude determination

KW - calibration

KW - identification

KW - mini-satellite

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U2 - 10.1016/j.ifacol.2015.09.153

DO - 10.1016/j.ifacol.2015.09.153

M3 - Article

AN - SCOPUS:84992511267

SN - 2405-8963

VL - 48

SP - 16

EP - 21

JO - IFAC-PapersOnLine

JF - IFAC-PapersOnLine

IS - 11 11

ER -

In-Flight Identification of Magnetometer and Attitude Determination System for Land-survey Mini-satellite

Abstract

Bibliographical note

Keywords

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