Thrust Vector Control of an Upper-Stage Rocket with Multiple Propellant Slosh Modes

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Thrust Vector Control of an Upper-Stage Rocket with Multiple Propellant Slosh Modes

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 pitchingmoment about the center of mass of the spacecraft. The rocket acceleration due to themain engine thrust is assumed to be large enough so that surface tension forces do not significantly affect the p...

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Clearance of Thrust Vector Control (TVC) laws for launchers demands the capability to provide analytical certificates for the system’s robust stability. During exo-atmospheric flight, a key role is played by the ability to deal with non rigid-body effects such as fuel sloshing. Depending on its frequency and magnitude, sloshing can easily deteriorate the performance of the TVC laws to the point...

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ژورنال

عنوان ژورنال: Mathematical Problems in Engineering

سال: 2012

ISSN: 1024-123X,1563-5147

DOI: 10.1155/2012/848741