Characterizing Observed Limit Cycles in the Cassini Main Engine Thrust Vector Control System

Author(s):  
Farheen Rizvi ◽  
Raquel Weitl
2012 ◽  
Vol 2012 ◽  
pp. 1-18 ◽  
Author(s):  
Jaime Rubio Hervas ◽  
Mahmut Reyhanoglu

The thrust vector control problem for an upper-stage rocket with propellant slosh dynamics is considered. The control inputs are defined by the gimbal deflection angle of a main engine and a pitching moment about the center of mass of the spacecraft. The rocket acceleration due to the main engine thrust is assumed to be large enough so that surface tension forces do not significantly affect the propellant motion during main engine burns. A multi-mass-spring model of the sloshing fuel is introduced to represent the prominent sloshing modes. A nonlinear feedback controller is designed to control the translational velocity vector and the attitude of the spacecraft, while suppressing the sloshing modes. The effectiveness of the controller is illustrated through a simulation example.


Author(s):  
Timo Wekerle ◽  
Euler Barbosa ◽  
Cesar M. Batagini ◽  
Luís E. Loures da Costa ◽  
Luís G. Trabasso

1995 ◽  
Author(s):  
Eiki Ishibashi ◽  
Shunichi Okaya ◽  
Takao Endo ◽  
Takumi Ujino

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