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- W4205403722 abstract "Rapid development of space technologies and their entrance to nano-level pulls out new demands for corresponding element base for manufacturing highly effective systems for angular control of the satellites. One of the most wide spread methods of angular stabilization and orientation of the space craft are systems in which reaction wheels are executive parts.While a control loop is being designed the main demand for a reaction wheel is to ensure that external control signal is proportional to created reaction momentum within all the rpm range of reaction wheel rotor.This article is dedicated to provision of control law stability for reaction wheel, built on the base of brushless direct current motor with slotless stator and pulse-duration modulation control with single PDM inverter for all the phases, for wide range of rpm by compensating phase coils’ inductance effect. Introduced approach allows compensating reaction wheel phase coils’ inductance effect on control law with preassigned accuracy and provides proportionality of reaction momentum of reaction-wheel and control signal within all the range of rpm for reaction wheel rotor." @default.
- W4205403722 created "2022-01-26" @default.
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- W4205403722 date "2013-12-23" @default.
- W4205403722 modified "2023-09-25" @default.
- W4205403722 title "THE INFLUENCE OF PHASE COILS’ INDUCTANCE EFFECT ON REACTION-WHEEL ACCURACY" @default.
- W4205403722 doi "https://doi.org/10.20535/0203-377126201330673" @default.
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