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...
| الحاوية / القاعدة: | فصلنامه علوم و فناوری فضایی |
|---|---|
| المؤلفون الرئيسيون: | , , |
| التنسيق: | مقال |
| اللغة: | الفارسية |
| منشور في: |
Aerospace Research Institute
2022-03-01
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| الموضوعات: | |
| الوصول للمادة أونلاين: | https://jsst.ias.ir/article_132801_8feab2a335f4ae75fa168c7d52fc1bf1.pdf |