8. Attitude Determination, Control, and Sensing

8.2 Subsystem Responsibilities

 

The flow of information for ADCS system.© Springer-Verlag Berlin Heidelberg 2014.

The Attitude Determination, Control, and Sensing (ADCS) system is responsible for the hardware and algorithms that estimate and control the spacecraft’s orientation. The ADCS system components are like the sensors and actuators of our body’s motor functions: the eyes, inner ear (for balance), nerves (sense of touch), arms, and core. The ADCS system is responsible for:

During the design process, the ADCS specialist:

  • selects sensors and actuators that ultimately yield precision pointing or tracking accuracy and precision.
  • conducts analysis on external and internal forces and torques to discover contributions to spacecraft dynamics due to these disturbances (common for spacecraft with components that vibrate). This may include dynamic simulation analysis.
  • coordinates with the structures and mechanisms specialist to place and mount sensors and actuators with unique requirements, like an unoccluded field of views or close placement to the center of mass.
  • calculates and codes algorithms to estimate position and attitude states, and also controls spacecraft attitude to the required accuracy and precision. This may include development within a simulation environment.
AA236: Overview of Spacecraft GN&C Subsystems Brian Howley Lockheed Martin Space Systems Company.

License

Icon for the Creative Commons Attribution 4.0 International License

A Guide to CubeSat Mission and Bus Design Copyright © by Frances Zhu is licensed under a Creative Commons Attribution 4.0 International License, except where otherwise noted.

Share This Book