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Paper Information

Journal:   INTERNATIONAL JOURNAL OF INDUSTRIAL ENGINEERING AND PRODUCTION MANAGEMENT (IJIE) (INTERNATIONAL JOURNAL OF ENGINEERING SCIENCE) (PERSIAN)   2004 , Volume 15 , Number 3; Page(s) 101 To 119.
 
Paper: 

VIBRATION AND DYNAMIC STABILITY ANALYSIS OF A LIQUID FUEL BALLISTIC MISSILE UNDER THE FUEL SLOSHING EFFECTS

 
 
Author(s):  REZAEI D., ESMAEILZADEH KHADEM S., MAHMOUDI S.N.
 
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Abstract: 

In this paper, the governing equations of motion for a liquid fuel rigid ballistic missile, by considering the fuel sloshing effect are derived. The missile performs under a guidance law control system. The external forces are due to aerodynamic and thrust forces and the sloshing effect in the linear range is modeled as simple mass-spring-damper system. In order to solve the equations of motion, in each time step, one needs to compute the motion variables for the missile dry- structure and the sloshing degree of freedom. Finally, the solution is obtained and the simulation results are presented in such a way that in each step motion variables of dry-structure and sloshing modes are calculated.

 
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