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

Department of Aeronautical Engineering

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

1 Citation (Scopus)

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.

Original language	English
Title of host publication	RAST 2015 - Proceedings of 7th International Conference on Recent Advances in Space Technologies
Editors	M. Fevzi Unal, Suleyman Basturk, Okyay Kaynak, Abdurrahman Hacioglu, Fuat Ince
Publisher	Institute of Electrical and Electronics Engineers Inc.
Pages	461-466
Number of pages	6
ISBN (Electronic)	9781467377607
DOIs	https://doi.org/10.1109/RAST.2015.7208389
Publication status	Published - 17 Aug 2015
Event	7th International Conference on Recent Advances in Space Technologies, RAST 2015 - Istanbul, Turkey Duration: 16 Jun 2015 → 19 Jun 2015

Publication series

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

Conference

Conference	7th International Conference on Recent Advances in Space Technologies, RAST 2015
Country/Territory	Turkey
City	Istanbul
Period	16/06/15 → 19/06/15

Bibliographical note

Publisher Copyright:
© 2015 IEEE.

Keywords

equivalent mechanical model
Lagrange equations
nonlinear dynamics
propellant slosh

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10.1109/RAST.2015.7208389

Cite this

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). Article 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. editor / 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).

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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",

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doi = "10.1109/RAST.2015.7208389",

language = "English",

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

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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).

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

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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, editors, 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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