10Nms control moment gyroscope
Product Introduction
The product is moved by the inner frameIt is composed of a measuring wheel assembly, a low-speed base assembly, and a circuit box controller assembly (including software), which generates a control moment by changing the direction of angular momentum (the angular momentum does not change) to achieve agile maneuvering of the satellite.
It is suitable for small and medium-sized satellite platforms with three-axis high-precision attitude and agile maneuver requirements
Product Features
Lightweight, high-precision frame low-speed control
FPGA-based control circuit, RS422 digital interface
High stiffness support, small micro-vibration
Momentum wheel weight reduction groove, long life of bearing assembly
Support customized production on demand.
