NASA NTRS · 19830000644
Mathematical Simulation of Flight Maneuvers
Abstract
Mathematical model simulates response of spin-stabilized spacecraft to commanded thruster pulses, using set of equations based on known inertial properties of vehicle and previously-determined thrustor performance. Model used to generate sequence of thrustor commands to accomplish specified maneuver.
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Frauenholz, R. B.. 1984-11-01. Mathematical Simulation of Flight Maneuvers. https://ntrs.nasa.gov/citations/19830000644
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