Performance comparison of guidance algorithms for asteroid intercept

Erdem Turan; Chingiz Hajiyev

doi:10.1109/RAST.2019.8767428

Performance comparison of guidance algorithms for asteroid intercept

Erdem Turan, Chingiz Hajiyev

Uçak Mühendisliği Bölümü

Istanbul Technical University

Araştırma sonucu: Kitap/Rapor/Konferans Bildirisinde Bölüm › Konferans katkısı › bilirkişi

2 Atıf (Scopus)

Özet

Linear quadratic one-sided optimized guidance laws and particle swarm optimization guidance law are investigated for hypervelocity asteroid intercept mission. Also, this paper examines the effect of noise on the line of sight measurements. In order to extract the actual value of the line of sight rate, the Kalman filter algorithm is used for certain guidance laws. Homing loop simulation results based upon Monte Carlo method show the effectiveness and accuracy of the various guidance laws.

Orijinal dil	İngilizce
Ana bilgisayar yayını başlığı	Proceedings of 9th International Conference on Recent Advances in Space Technologies, RAST 2019
Editörler	S. Menekay, O. Cetin, O. Alparslan
Yayınlayan	Institute of Electrical and Electronics Engineers Inc.
Sayfalar	919-925
Sayfa sayısı	7
ISBN (Elektronik)	9781538694480
DOI'lar	https://doi.org/10.1109/RAST.2019.8767428
Yayın durumu	Yayınlandı - Haz 2019
Etkinlik	9th International Conference on Recent Advances in Space Technologies, RAST 2019 - Istanbul, Turkey Süre: 11 Haz 2019 → 14 Haz 2019

Yayın serisi

Adı	Proceedings of 9th International Conference on Recent Advances in Space Technologies, RAST 2019

???event.eventtypes.event.conference???

???event.eventtypes.event.conference???	9th International Conference on Recent Advances in Space Technologies, RAST 2019
Ülke/Bölge	Turkey
Şehir	Istanbul
Periyot	11/06/19 → 14/06/19

Bibliyografik not

Publisher Copyright:
© 2019 IEEE.

Belgeye Erişim

10.1109/RAST.2019.8767428

Diğer Dosyalar ve Linkler

Link to publication in Scopus

Alıntı Yap

Turan, E., & Hajiyev, C. (2019). Performance comparison of guidance algorithms for asteroid intercept. In S. Menekay, O. Cetin, & O. Alparslan (Eds.), Proceedings of 9th International Conference on Recent Advances in Space Technologies, RAST 2019 (pp. 919-925). Makale 8767428 (Proceedings of 9th International Conference on Recent Advances in Space Technologies, RAST 2019). Institute of Electrical and Electronics Engineers Inc.. https://doi.org/10.1109/RAST.2019.8767428

Turan, Erdem ; Hajiyev, Chingiz. / Performance comparison of guidance algorithms for asteroid intercept. Proceedings of 9th International Conference on Recent Advances in Space Technologies, RAST 2019. editör / S. Menekay ; O. Cetin ; O. Alparslan. Institute of Electrical and Electronics Engineers Inc., 2019. pp. 919-925 (Proceedings of 9th International Conference on Recent Advances in Space Technologies, RAST 2019).

@inproceedings{7b27409ac0864d8b9eb8eea6378b7737,

title = "Performance comparison of guidance algorithms for asteroid intercept",

abstract = "Linear quadratic one-sided optimized guidance laws and particle swarm optimization guidance law are investigated for hypervelocity asteroid intercept mission. Also, this paper examines the effect of noise on the line of sight measurements. In order to extract the actual value of the line of sight rate, the Kalman filter algorithm is used for certain guidance laws. Homing loop simulation results based upon Monte Carlo method show the effectiveness and accuracy of the various guidance laws.",

keywords = "guidance, intercept, kalman filter, navigation",

author = "Erdem Turan and Chingiz Hajiyev",

note = "Publisher Copyright: {\textcopyright} 2019 IEEE.; 9th International Conference on Recent Advances in Space Technologies, RAST 2019 ; Conference date: 11-06-2019 Through 14-06-2019",

year = "2019",

month = jun,

doi = "10.1109/RAST.2019.8767428",

language = "English",

series = "Proceedings of 9th International Conference on Recent Advances in Space Technologies, RAST 2019",

publisher = "Institute of Electrical and Electronics Engineers Inc.",

pages = "919--925",

editor = "S. Menekay and O. Cetin and O. Alparslan",

booktitle = "Proceedings of 9th International Conference on Recent Advances in Space Technologies, RAST 2019",

address = "United States",

}

Turan, E & Hajiyev, C 2019, Performance comparison of guidance algorithms for asteroid intercept. in S Menekay, O Cetin & O Alparslan (eds), Proceedings of 9th International Conference on Recent Advances in Space Technologies, RAST 2019., 8767428, Proceedings of 9th International Conference on Recent Advances in Space Technologies, RAST 2019, Institute of Electrical and Electronics Engineers Inc., pp. 919-925, 9th International Conference on Recent Advances in Space Technologies, RAST 2019, Istanbul, Turkey, 11/06/19. https://doi.org/10.1109/RAST.2019.8767428

Performance comparison of guidance algorithms for asteroid intercept. / Turan, Erdem; Hajiyev, Chingiz.
Proceedings of 9th International Conference on Recent Advances in Space Technologies, RAST 2019. ed. / S. Menekay; O. Cetin; O. Alparslan. Institute of Electrical and Electronics Engineers Inc., 2019. p. 919-925 8767428 (Proceedings of 9th International Conference on Recent Advances in Space Technologies, RAST 2019).

Araştırma sonucu: Kitap/Rapor/Konferans Bildirisinde Bölüm › Konferans katkısı › bilirkişi

TY - GEN

T1 - Performance comparison of guidance algorithms for asteroid intercept

AU - Turan, Erdem

AU - Hajiyev, Chingiz

PY - 2019/6

Y1 - 2019/6

N2 - Linear quadratic one-sided optimized guidance laws and particle swarm optimization guidance law are investigated for hypervelocity asteroid intercept mission. Also, this paper examines the effect of noise on the line of sight measurements. In order to extract the actual value of the line of sight rate, the Kalman filter algorithm is used for certain guidance laws. Homing loop simulation results based upon Monte Carlo method show the effectiveness and accuracy of the various guidance laws.

AB - Linear quadratic one-sided optimized guidance laws and particle swarm optimization guidance law are investigated for hypervelocity asteroid intercept mission. Also, this paper examines the effect of noise on the line of sight measurements. In order to extract the actual value of the line of sight rate, the Kalman filter algorithm is used for certain guidance laws. Homing loop simulation results based upon Monte Carlo method show the effectiveness and accuracy of the various guidance laws.

KW - guidance

KW - intercept

KW - kalman filter

KW - navigation

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U2 - 10.1109/RAST.2019.8767428

DO - 10.1109/RAST.2019.8767428

M3 - Conference contribution

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T3 - Proceedings of 9th International Conference on Recent Advances in Space Technologies, RAST 2019

SP - 919

EP - 925

BT - Proceedings of 9th International Conference on Recent Advances in Space Technologies, RAST 2019

A2 - Menekay, S.

A2 - Cetin, O.

A2 - Alparslan, O.

PB - Institute of Electrical and Electronics Engineers Inc.

T2 - 9th International Conference on Recent Advances in Space Technologies, RAST 2019

Y2 - 11 June 2019 through 14 June 2019

ER -

Turan E, Hajiyev C. Performance comparison of guidance algorithms for asteroid intercept. In Menekay S, Cetin O, Alparslan O, editörler, Proceedings of 9th International Conference on Recent Advances in Space Technologies, RAST 2019. Institute of Electrical and Electronics Engineers Inc. 2019. p. 919-925. 8767428. (Proceedings of 9th International Conference on Recent Advances in Space Technologies, RAST 2019). doi: 10.1109/RAST.2019.8767428

Performance comparison of guidance algorithms for asteroid intercept

Özet

Yayın serisi

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Bibliyografik not

Belgeye Erişim

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