Thrust vector control of an upper-stage rocket with multiple propellant slosh modes

DOI10.1155/2012/848741zbMath1264.93078OpenAlexW2104081297WikidataQ58912230 ScholiaQ58912230MaRDI QIDQ1955266

Jaime Rubio Hervas, Mahmut Reyhanoglu

Publication date: 11 June 2013

Published in: Mathematical Problems in Engineering (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1155/2012/848741

Mathematics Subject Classification ID

Stabilization of systems by feedback (93D15) Nonlinear systems in control theory (93C10) Control of mechanical systems (70Q05)

Related Items (1)

Development and verification of a flexible tethered satellite system model considering the fuel slosh

Cites Work

• Unnamed Item
• Attitude stabilization of a rigid spacecraft using two control torques: A nonlinear control approach based on the spacecraft attitude dynamics
• Controllability and point-to-point control of 3-DOF planar horizontal underactuated manipulators
• Discontinuous feedback control of a special class of underactuated mechanical systems

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