Ever since the launch of the early high-efficiency rockets, controlling liquid fuel slosh within a launch vehicle has been a major design concern. Moreover, with today\u27s large and complex spacecraft, a substantial mass of fuel is necessary to place them into orbit and to perform orbital maneuvers. --From the book\u27s introduction
This paper studies the thrust vector control problem for an upper-stage rocket with fuel slosh dynam...
The modeling of the liquid dynamics within the tanks of liquid-propelled vehicles is presented in th...
We study control problems for planar maneuvers of a spacecraft with fuel slosh in a zero gravity env...
Ever since the launch of the early high-efficiency rockets, controlling liquid fuel slosh within a l...
In April of 1957, a Jupiter Intermediate Range Ballistic Missile was terminated 90 seconds after lau...
This paper studies the modeling and control problem for planar maneuvering of space vehicles with fu...
This open access book is published by InTech, a publisher of open access books and journals in the f...
International audienceThe design of challenging and ambitious space missions entails a tightening of...
International audienceThe design of challenging and ambitious space missions entails a tightening of...
Modern spacecraft often contain large quantities of liquid fuel to execute station keeping and attit...
Liquid sloshing within spacecraft propellant tanks causes rapid energy dissipation at resonant modes...
One of the challenges of developing flight control systems for liquid-propelled space vehicles is en...
We develop a mathematical model that describes the accelerating flight of a spacecraft in a fixed pl...
During thrust maneuvers, the sloshing of fuel in partially filled tanks could interact with the cont...
“The thrust vector control problem for an upper-stage rocket with propellant slosh dynamics is consi...
This paper studies the thrust vector control problem for an upper-stage rocket with fuel slosh dynam...
The modeling of the liquid dynamics within the tanks of liquid-propelled vehicles is presented in th...
We study control problems for planar maneuvers of a spacecraft with fuel slosh in a zero gravity env...
Ever since the launch of the early high-efficiency rockets, controlling liquid fuel slosh within a l...
In April of 1957, a Jupiter Intermediate Range Ballistic Missile was terminated 90 seconds after lau...
This paper studies the modeling and control problem for planar maneuvering of space vehicles with fu...
This open access book is published by InTech, a publisher of open access books and journals in the f...
International audienceThe design of challenging and ambitious space missions entails a tightening of...
International audienceThe design of challenging and ambitious space missions entails a tightening of...
Modern spacecraft often contain large quantities of liquid fuel to execute station keeping and attit...
Liquid sloshing within spacecraft propellant tanks causes rapid energy dissipation at resonant modes...
One of the challenges of developing flight control systems for liquid-propelled space vehicles is en...
We develop a mathematical model that describes the accelerating flight of a spacecraft in a fixed pl...
During thrust maneuvers, the sloshing of fuel in partially filled tanks could interact with the cont...
“The thrust vector control problem for an upper-stage rocket with propellant slosh dynamics is consi...
This paper studies the thrust vector control problem for an upper-stage rocket with fuel slosh dynam...
The modeling of the liquid dynamics within the tanks of liquid-propelled vehicles is presented in th...
We study control problems for planar maneuvers of a spacecraft with fuel slosh in a zero gravity env...