Attitude control

Attitude control in spacecraft refers to the systems and methods used to precisely orient the spacecraft in space. This involves adjusting its pitch, yaw, and roll—similar to how a car or airplane can turn or tilt—so it points in the desired direction for tasks like communication, observation, or navigation. Attitude control uses sensors to determine the spacecraft’s orientation and actuators such as thrusters, reaction wheels, or control moment gyroscopes to make adjustments. Maintaining proper attitude ensures the spacecraft’s instruments and antennas are correctly aligned, optimizing their performance and mission success.