Vibration Control Design of Fuel Sloshing in a Spacecraft Using Virtual Actuator
This paper is dedicated to modeling of fuel sloshing dynamics and its effect on the stability and control of the space vehicle. Sloshing due to the liquid movement in the fuel tank of a space vehicle's propulsion system can be effective on the vehicle’s control and stability. Force and moment i...
| 發表在: | فصلنامه علوم و فناوری فضایی |
|---|---|
| Main Authors: | , , |
| 格式: | Article |
| 語言: | 波斯语 |
| 出版: |
Aerospace Research Institute
2022-03-01
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| 主題: | |
| 在線閱讀: | https://jsst.ias.ir/article_132801_8feab2a335f4ae75fa168c7d52fc1bf1.pdf |
| _version_ | 1850066493703716864 |
|---|---|
| author | Abdolmajid khoshnood Ali Aminzadeh Peyman Nikpey |
| author_facet | Abdolmajid khoshnood Ali Aminzadeh Peyman Nikpey |
| author_sort | Abdolmajid khoshnood |
| collection | DOAJ |
| container_title | فصلنامه علوم و فناوری فضایی |
| description | This paper is dedicated to modeling of fuel sloshing dynamics and its effect on the stability and control of the space vehicle. Sloshing due to the liquid movement in the fuel tank of a space vehicle's propulsion system can be effective on the vehicle’s control and stability. Force and moment interaction between fuel sloshing and space vehicle’s control system will be appeared as a feedback in the control system. With respect to simplicity of analyzing of a rigid body's equations of motion in comparison with a fluid dynamics equations and as a result reducing computational efforts, it is possible to apply a mechanical model instead. So in this paper fuel sloshing is modelled as a linear mechanical system to investigate its effect on the stability and control of the vehicle. For this purpose, two mechanical models, mass-spring and pendulum systems, are applied to model dynamics of a space vehicle with fuel sloshing and each system’s parameters are evaluated for simulat |
| format | Article |
| id | doaj-art-28714d396f2b45a8a02407eb545647aa |
| institution | Directory of Open Access Journals |
| issn | 2008-4560 2423-4516 |
| language | fas |
| publishDate | 2022-03-01 |
| publisher | Aerospace Research Institute |
| record_format | Article |
| spelling | doaj-art-28714d396f2b45a8a02407eb545647aa2025-08-20T00:19:18ZfasAerospace Research Instituteفصلنامه علوم و فناوری فضایی2008-45602423-45162022-03-01151637110.30699/jsst.2021.1326132801Vibration Control Design of Fuel Sloshing in a Spacecraft Using Virtual ActuatorAbdolmajid khoshnood0Ali Aminzadeh1Peyman Nikpey2Associate Professor, Faculty of Aerospace Engineering, K.N. Toosi University of Technology, Tehran, IranPh.D. Student, Department of Aerospace Engineering, K.N. Toosi University of Technology, Tehran, IranEducator, Satellite Research Institute, Iranian Research Center, Tehran, IranThis paper is dedicated to modeling of fuel sloshing dynamics and its effect on the stability and control of the space vehicle. Sloshing due to the liquid movement in the fuel tank of a space vehicle's propulsion system can be effective on the vehicle’s control and stability. Force and moment interaction between fuel sloshing and space vehicle’s control system will be appeared as a feedback in the control system. With respect to simplicity of analyzing of a rigid body's equations of motion in comparison with a fluid dynamics equations and as a result reducing computational efforts, it is possible to apply a mechanical model instead. So in this paper fuel sloshing is modelled as a linear mechanical system to investigate its effect on the stability and control of the vehicle. For this purpose, two mechanical models, mass-spring and pendulum systems, are applied to model dynamics of a space vehicle with fuel sloshing and each system’s parameters are evaluated for simulathttps://jsst.ias.ir/article_132801_8feab2a335f4ae75fa168c7d52fc1bf1.pdffuel sloshingspacecraftmass-spring modelvirtual actuatorlqr |
| spellingShingle | Abdolmajid khoshnood Ali Aminzadeh Peyman Nikpey Vibration Control Design of Fuel Sloshing in a Spacecraft Using Virtual Actuator fuel sloshing spacecraft mass-spring model virtual actuator lqr |
| title | Vibration Control Design of Fuel Sloshing in a Spacecraft Using Virtual Actuator |
| title_full | Vibration Control Design of Fuel Sloshing in a Spacecraft Using Virtual Actuator |
| title_fullStr | Vibration Control Design of Fuel Sloshing in a Spacecraft Using Virtual Actuator |
| title_full_unstemmed | Vibration Control Design of Fuel Sloshing in a Spacecraft Using Virtual Actuator |
| title_short | Vibration Control Design of Fuel Sloshing in a Spacecraft Using Virtual Actuator |
| title_sort | vibration control design of fuel sloshing in a spacecraft using virtual actuator |
| topic | fuel sloshing spacecraft mass-spring model virtual actuator lqr |
| url | https://jsst.ias.ir/article_132801_8feab2a335f4ae75fa168c7d52fc1bf1.pdf |
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