Model and control problem for space vehicles with propellant slosh

Merve Sahin; Melahat Cihan; Metin Orhan Kaya

doi:10.1109/RAST.2015.7208389

Model and control problem for space vehicles with propellant slosh

Merve Sahin, Melahat Cihan, Metin Orhan Kaya

Uçak Mühendisliği Bölümü

Araştırma sonucu: ???type-name??? › Konferans katkısı › bilirkişi

1 Atıf (Scopus)

Özet

This paper contains calculations about propellant slosh for an upper stage rocket. The liquid fuel is modeled by using an equivalent mechanical model, from this point of view the stability of this rocket is examined by means of mass-spring model. In theory, a nonlinear mathematical model is derived and nonlinear feedback control laws are used. Specifications of the Attitude Vernier Upper Module (AVUM) upper stage rocket Vega are chosen for simulations. The results of this study are obtained for first four slosh modes.

Orijinal dil	İngilizce
Ana bilgisayar yayını başlığı	RAST 2015 - Proceedings of 7th International Conference on Recent Advances in Space Technologies
Editörler	M. Fevzi Unal, Suleyman Basturk, Okyay Kaynak, Abdurrahman Hacioglu, Fuat Ince
Yayınlayan	Institute of Electrical and Electronics Engineers Inc.
Sayfalar	461-466
Sayfa sayısı	6
ISBN (Elektronik)	9781467377607
DOI'lar	https://doi.org/10.1109/RAST.2015.7208389
Yayın durumu	Yayınlandı - 17 Ağu 2015
Etkinlik	7th International Conference on Recent Advances in Space Technologies, RAST 2015 - Istanbul, Turkey Süre: 16 Haz 2015 → 19 Haz 2015

Yayın serisi

Adı	RAST 2015 - Proceedings of 7th International Conference on Recent Advances in Space Technologies

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

???event.eventtypes.event.conference???	7th International Conference on Recent Advances in Space Technologies, RAST 2015
Ülke/Bölge	Turkey
Şehir	Istanbul
Periyot	16/06/15 → 19/06/15

Bibliyografik not

Publisher Copyright:
© 2015 IEEE.

Belgeye Erişim

10.1109/RAST.2015.7208389

Diğer Dosyalar ve Linkler

Link to publication in Scopus

Alıntı Yap

Sahin, M., Cihan, M., & Kaya, M. O. (2015). Model and control problem for space vehicles with propellant slosh. In M. F. Unal, S. Basturk, O. Kaynak, A. Hacioglu, & F. Ince (Eds.), RAST 2015 - Proceedings of 7th International Conference on Recent Advances in Space Technologies (pp. 461-466). Makale 7208389 (RAST 2015 - Proceedings of 7th International Conference on Recent Advances in Space Technologies). Institute of Electrical and Electronics Engineers Inc.. https://doi.org/10.1109/RAST.2015.7208389

Sahin, Merve ; Cihan, Melahat ; Kaya, Metin Orhan. / Model and control problem for space vehicles with propellant slosh. RAST 2015 - Proceedings of 7th International Conference on Recent Advances in Space Technologies. editör / M. Fevzi Unal ; Suleyman Basturk ; Okyay Kaynak ; Abdurrahman Hacioglu ; Fuat Ince. Institute of Electrical and Electronics Engineers Inc., 2015. pp. 461-466 (RAST 2015 - Proceedings of 7th International Conference on Recent Advances in Space Technologies).

@inproceedings{13525c7bb0c6440a86602b03adf373ab,

title = "Model and control problem for space vehicles with propellant slosh",

abstract = "This paper contains calculations about propellant slosh for an upper stage rocket. The liquid fuel is modeled by using an equivalent mechanical model, from this point of view the stability of this rocket is examined by means of mass-spring model. In theory, a nonlinear mathematical model is derived and nonlinear feedback control laws are used. Specifications of the Attitude Vernier Upper Module (AVUM) upper stage rocket Vega are chosen for simulations. The results of this study are obtained for first four slosh modes.",

keywords = "equivalent mechanical model, Lagrange equations, nonlinear dynamics, propellant slosh",

author = "Merve Sahin and Melahat Cihan and Kaya, {Metin Orhan}",

note = "Publisher Copyright: {\textcopyright} 2015 IEEE.; 7th International Conference on Recent Advances in Space Technologies, RAST 2015 ; Conference date: 16-06-2015 Through 19-06-2015",

year = "2015",

month = aug,

day = "17",

doi = "10.1109/RAST.2015.7208389",

language = "English",

series = "RAST 2015 - Proceedings of 7th International Conference on Recent Advances in Space Technologies",

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

pages = "461--466",

editor = "Unal, {M. Fevzi} and Suleyman Basturk and Okyay Kaynak and Abdurrahman Hacioglu and Fuat Ince",

booktitle = "RAST 2015 - Proceedings of 7th International Conference on Recent Advances in Space Technologies",

address = "United States",

}

Sahin, M, Cihan, M & Kaya, MO 2015, Model and control problem for space vehicles with propellant slosh. in MF Unal, S Basturk, O Kaynak, A Hacioglu & F Ince (eds), RAST 2015 - Proceedings of 7th International Conference on Recent Advances in Space Technologies., 7208389, RAST 2015 - Proceedings of 7th International Conference on Recent Advances in Space Technologies, Institute of Electrical and Electronics Engineers Inc., pp. 461-466, 7th International Conference on Recent Advances in Space Technologies, RAST 2015, Istanbul, Turkey, 16/06/15. https://doi.org/10.1109/RAST.2015.7208389

Model and control problem for space vehicles with propellant slosh. / Sahin, Merve; Cihan, Melahat; Kaya, Metin Orhan.
RAST 2015 - Proceedings of 7th International Conference on Recent Advances in Space Technologies. ed. / M. Fevzi Unal; Suleyman Basturk; Okyay Kaynak; Abdurrahman Hacioglu; Fuat Ince. Institute of Electrical and Electronics Engineers Inc., 2015. p. 461-466 7208389 (RAST 2015 - Proceedings of 7th International Conference on Recent Advances in Space Technologies).

Araştırma sonucu: ???type-name??? › Konferans katkısı › bilirkişi

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AU - Cihan, Melahat

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PY - 2015/8/17

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N2 - This paper contains calculations about propellant slosh for an upper stage rocket. The liquid fuel is modeled by using an equivalent mechanical model, from this point of view the stability of this rocket is examined by means of mass-spring model. In theory, a nonlinear mathematical model is derived and nonlinear feedback control laws are used. Specifications of the Attitude Vernier Upper Module (AVUM) upper stage rocket Vega are chosen for simulations. The results of this study are obtained for first four slosh modes.

AB - This paper contains calculations about propellant slosh for an upper stage rocket. The liquid fuel is modeled by using an equivalent mechanical model, from this point of view the stability of this rocket is examined by means of mass-spring model. In theory, a nonlinear mathematical model is derived and nonlinear feedback control laws are used. Specifications of the Attitude Vernier Upper Module (AVUM) upper stage rocket Vega are chosen for simulations. The results of this study are obtained for first four slosh modes.

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Sahin M, Cihan M, Kaya MO. Model and control problem for space vehicles with propellant slosh. In Unal MF, Basturk S, Kaynak O, Hacioglu A, Ince F, editörler, RAST 2015 - Proceedings of 7th International Conference on Recent Advances in Space Technologies. Institute of Electrical and Electronics Engineers Inc. 2015. p. 461-466. 7208389. (RAST 2015 - Proceedings of 7th International Conference on Recent Advances in Space Technologies). doi: 10.1109/RAST.2015.7208389

Model and control problem for space vehicles with propellant slosh

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