SUMMARY
A reaction wheel is a crucial component in satellite attitude control, particularly in CubeSats, where it utilizes angular momentum to control orientation. Typically, satellites employ three to four reaction wheels, with the fourth wheel providing redundancy. When a wheel reaches maximum speed, known as saturation, it requires a desaturation burn using thrusters to maintain course. Reaction wheels are more fuel-efficient than constant thruster firings for satellite pointing, although their mass limits their use in smaller CubeSats.
PREREQUISITES
- Understanding of satellite attitude control systems
- Familiarity with angular momentum principles
- Knowledge of CubeSat design and limitations
- Basic concepts of torque and rotational dynamics
NEXT STEPS
- Research the design and function of CubeSat attitude determination and control units
- Explore the principles of angular momentum and its application in reaction wheels
- Learn about desaturation techniques and their importance in satellite operations
- Investigate the differences between reaction wheels and other attitude control methods, such as thrusters and magnetic torque coils
USEFUL FOR
Engineers and researchers involved in satellite design, particularly those focusing on CubeSat projects, as well as students studying aerospace engineering and satellite technology.