A momentum wheel is a flywheel spun at high constant speed to give a satellite gyroscopic stiffness — resistance to being twisted off its pointing. Where reaction wheels vary speed to steer, momentum wheels hold a bias, stabilising spin-averse designs like classic GEO comsats.
Understanding Momentum Wheel
Gyroscopic stiffness, quantified
Stored momentum H turns a disturbance torque T into a slow precession at rate T/H instead of an accelerating tumble. Size H so that worst-case torques precess the platform slower than the control loop's correction cadence, and pointing becomes serene: the spacecraft glides through disturbances that would demand constant wheel activity in a zero-bias design. The cost is manoeuvre stubbornness — the same stiffness resists commanded turns, so momentum-bias craft slew like tankers.
Architectures across eras
Spin-stabilised satellites (the whole body as flywheel) began the lineage; dual-spin designs de-spun an antenna platform atop a spinning drum; momentum-bias three-axis control refined it; and today's four-wheel zero-bias clusters complete the shift to agility, with control moment gyroscopes — gimballed momentum wheels whose tilt produces large torques — powering the fastest slewing imagers and stations. Each step trades passive stability for commanded authority.