Attitude determination and rotational motion parameters identification of a LEO satellite through magnetometer and sun sensor data

A. Kutlu; Ch Haciyev; O. Tekinalp

doi:10.1109/RAST.2007.4284033

Attitude determination and rotational motion parameters identification of a LEO satellite through magnetometer and sun sensor data

A. Kutlu^*, Ch Haciyev, O. Tekinalp

^*Corresponding author for this work

Department of Aeronautical Engineering

Middle East Technical University

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

15 Citations (Scopus)

Abstract

In this paper, Attitude Determination and Parameter Identification problem of a LEO satellite are studied. In Attitude Determination System three rate gyroscopes, three axis magnetometer and a sun sensor data are used. Using Kalman Filter algorithms angular rates and quaternions are estimated. In these algorithms, rate gyroscope bias measurements are also taken into consideration in state estimation. In Parameter Identification part, the Moment of Inertia values of the satellite are estimated by using Least Square Estimation method. Finally by combining these two parts, the Attitude and MoI values of the spacecraft are obtained.

Original language	English
Title of host publication	Proceedings of the 3rd International Conference on Recent Advances in Space Technologies, RAST 2007
Pages	458-461
Number of pages	4
DOIs	https://doi.org/10.1109/RAST.2007.4284033
Publication status	Published - 2007
Event	3rd International Conference on Recent Advances in Space Technologies, RAST 2007 - Istanbul, Turkey Duration: 14 Jun 2007 → 16 Jun 2007

Publication series

Name	Proceedings of the 3rd International Conference on Recent Advances in Space Technologies, RAST 2007

Conference

Conference	3rd International Conference on Recent Advances in Space Technologies, RAST 2007
Country/Territory	Turkey
City	Istanbul
Period	14/06/07 → 16/06/07

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10.1109/RAST.2007.4284033

Cite this

Kutlu, A., Haciyev, C., & Tekinalp, O. (2007). Attitude determination and rotational motion parameters identification of a LEO satellite through magnetometer and sun sensor data. In Proceedings of the 3rd International Conference on Recent Advances in Space Technologies, RAST 2007 (pp. 458-461). Article 4284033 (Proceedings of the 3rd International Conference on Recent Advances in Space Technologies, RAST 2007). https://doi.org/10.1109/RAST.2007.4284033

Kutlu, A. ; Haciyev, Ch ; Tekinalp, O. / Attitude determination and rotational motion parameters identification of a LEO satellite through magnetometer and sun sensor data. Proceedings of the 3rd International Conference on Recent Advances in Space Technologies, RAST 2007. 2007. pp. 458-461 (Proceedings of the 3rd International Conference on Recent Advances in Space Technologies, RAST 2007).

@inproceedings{d4b83a0dfd1b42a99ebf1c3376196911,

title = "Attitude determination and rotational motion parameters identification of a LEO satellite through magnetometer and sun sensor data",

abstract = "In this paper, Attitude Determination and Parameter Identification problem of a LEO satellite are studied. In Attitude Determination System three rate gyroscopes, three axis magnetometer and a sun sensor data are used. Using Kalman Filter algorithms angular rates and quaternions are estimated. In these algorithms, rate gyroscope bias measurements are also taken into consideration in state estimation. In Parameter Identification part, the Moment of Inertia values of the satellite are estimated by using Least Square Estimation method. Finally by combining these two parts, the Attitude and MoI values of the spacecraft are obtained.",

author = "A. Kutlu and Ch Haciyev and O. Tekinalp",

year = "2007",

doi = "10.1109/RAST.2007.4284033",

language = "English",

isbn = "1424410576",

series = "Proceedings of the 3rd International Conference on Recent Advances in Space Technologies, RAST 2007",

pages = "458--461",

booktitle = "Proceedings of the 3rd International Conference on Recent Advances in Space Technologies, RAST 2007",

note = "3rd International Conference on Recent Advances in Space Technologies, RAST 2007 ; Conference date: 14-06-2007 Through 16-06-2007",

}

Kutlu, A, Haciyev, C & Tekinalp, O 2007, Attitude determination and rotational motion parameters identification of a LEO satellite through magnetometer and sun sensor data. in Proceedings of the 3rd International Conference on Recent Advances in Space Technologies, RAST 2007., 4284033, Proceedings of the 3rd International Conference on Recent Advances in Space Technologies, RAST 2007, pp. 458-461, 3rd International Conference on Recent Advances in Space Technologies, RAST 2007, Istanbul, Turkey, 14/06/07. https://doi.org/10.1109/RAST.2007.4284033

Attitude determination and rotational motion parameters identification of a LEO satellite through magnetometer and sun sensor data. / Kutlu, A.; Haciyev, Ch; Tekinalp, O.
Proceedings of the 3rd International Conference on Recent Advances in Space Technologies, RAST 2007. 2007. p. 458-461 4284033 (Proceedings of the 3rd International Conference on Recent Advances in Space Technologies, RAST 2007).

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

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T1 - Attitude determination and rotational motion parameters identification of a LEO satellite through magnetometer and sun sensor data

AU - Kutlu, A.

AU - Haciyev, Ch

AU - Tekinalp, O.

PY - 2007

Y1 - 2007

N2 - In this paper, Attitude Determination and Parameter Identification problem of a LEO satellite are studied. In Attitude Determination System three rate gyroscopes, three axis magnetometer and a sun sensor data are used. Using Kalman Filter algorithms angular rates and quaternions are estimated. In these algorithms, rate gyroscope bias measurements are also taken into consideration in state estimation. In Parameter Identification part, the Moment of Inertia values of the satellite are estimated by using Least Square Estimation method. Finally by combining these two parts, the Attitude and MoI values of the spacecraft are obtained.

AB - In this paper, Attitude Determination and Parameter Identification problem of a LEO satellite are studied. In Attitude Determination System three rate gyroscopes, three axis magnetometer and a sun sensor data are used. Using Kalman Filter algorithms angular rates and quaternions are estimated. In these algorithms, rate gyroscope bias measurements are also taken into consideration in state estimation. In Parameter Identification part, the Moment of Inertia values of the satellite are estimated by using Least Square Estimation method. Finally by combining these two parts, the Attitude and MoI values of the spacecraft are obtained.

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U2 - 10.1109/RAST.2007.4284033

DO - 10.1109/RAST.2007.4284033

M3 - Conference contribution

AN - SCOPUS:46449111191

SN - 1424410576

SN - 9781424410576

T3 - Proceedings of the 3rd International Conference on Recent Advances in Space Technologies, RAST 2007

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BT - Proceedings of the 3rd International Conference on Recent Advances in Space Technologies, RAST 2007

T2 - 3rd International Conference on Recent Advances in Space Technologies, RAST 2007

Y2 - 14 June 2007 through 16 June 2007

ER -

Kutlu A, Haciyev C, Tekinalp O. Attitude determination and rotational motion parameters identification of a LEO satellite through magnetometer and sun sensor data. In Proceedings of the 3rd International Conference on Recent Advances in Space Technologies, RAST 2007. 2007. p. 458-461. 4284033. (Proceedings of the 3rd International Conference on Recent Advances in Space Technologies, RAST 2007). doi: 10.1109/RAST.2007.4284033

Attitude determination and rotational motion parameters identification of a LEO satellite through magnetometer and sun sensor data

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