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.
Mathematical Simulation of Flight Maneuvers
NASA Tech Briefs ; 8 , 2
01.11.1984
Sonstige
Keine Angabe
Englisch
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