EN
Suitable for medium and small satellite platforms that require three axis high precision attitude agile maneuvering.
Introduction:
Introduction:
This product consists of an inner frame momentum wheel component, a low-speed base component, and a circuit box controller component (including software). By changing the direction of angular momentum (with constant magnitude), control torque is generated to achieve agile maneuverability of the satellite.
Features:
Lightweight, high-precision framework for low-speed control;
Control circuit based on FPGA, RS422 digital interface;
High stiffness support, small vibration momentum level;
Momentum wheel weight reduction groove, long service life of bearing components;
Support customized production on demand.