Unified spacecraft attitude control system with pseudo-...
Unified spacecraft attitude control system with pseudo- complementary paired thrusters
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Method for low-fuel, computer-assisted control of any number...
determined number of thrusters, arranged as desired on a spacecraft, is to be specified, which method solves this linear optimization problem within
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METHOD FOR LOW-FUEL, COMPUTER-ASSISTED CONTROL OF ANY NUMBER...
METHOD FOR LOW-FUEL, COMPUTER-ASSISTED CONTROL OF ANY NUMBER OF THRUSTERS ARRANGED ON A SPACECRAFT
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Linear gridless ion thruster
A linear gridless ion thruster (LGIT) is provided to serve as an ion source for spacecraft propulsion or plasma processing.
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Linear gridless ion thruster
A linear gridless ion thruster (LGIT) is provided to serve as an ion source for spacecraft propulsion or plasma processing.
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LINEAR GRIDLESS ION THRUSTER
A linear gridless ion thruster (LGIT) is provided to serve as an ion source for spacecraft propulsion or plasma processing.
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Low power, linear geometry hall plasma source with an open...
Low power, linear geometry hall plasma source with an open electron drift
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Thruster optimized pair selection
a controller for calculating thrust forces comprises a plurality of thrusters disposed on said spacecraft in a spaced relationship relative to one
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Spacecraft attitude and velocity control system
F and a torque vector T, each having three orthogonal components, which represent the forces and torques which are to be generated by the thrusters.
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Interconnection of machine for effecting multiple orientation...
Interconnection of machine for effecting multiple orientation of linear motion slides
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Interconnection of machine for effecting multiple orientation...
Interconnection of machine for effecting multiple orientation of linear motion slides
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Attitude control system for momentum-biased spacecraft
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DRIVE UNIT FOR ADJUSTING SATELLITE COMPONENTS REQUIRING...
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Method for measuring the mass of liquid in a storage tank
heat depends upon the mass or amount of liquid in the tank, but a linear relationship is established between total mass and the product of total mass
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Drive unit for adjusting satellite components requiring...
satellite components requiring orientation such as thrusts includes two linear drives on which steering rods are articulated via gimbals.
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Method for the fuel-optimized selection of a thruster...
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