Guidance, Navigation, & Control (GNC)

GNC in One Loop (Sense → Estimate → Decide → Act)

GNC is the system that keeps spacecraft pointed correctly, on the right path, and stable under disturbances. In simple terms: it is how spacecraft “knows where it is” and “keeps itself on track.”

  • Guidance: compute a desired trajectory or attitude profile.
  • Navigation: estimate state (position, velocity, attitude) from sensors.
  • Control: command actuators to track the target and reject disturbances.

Attitude Determination & Control (ADCS)

ADCS focuses on orientation in 3D: pointing antennas, instruments, solar arrays, and performing maneuvers.

  • Actuators: reaction wheels, control moment gyros, magnetic torquers, thrusters.
  • Sensors: star trackers, sun sensors, IMUs/gyros, magnetometers, horizon sensors.
  • Avionics: flight software, control loops, redundancy management.

Disturbances and Error Sources

  • Environmental torques: gravity gradient, aerodynamic drag (LEO), SRP, magnetic interactions.
  • Sensor errors: bias, noise, misalignment, dropouts.
  • Actuator limits: saturation, wheel momentum buildup, thruster minimum impulse bit.

Modern Focus (Autonomy and Onboard Intelligence)

  • AI-based autonomous navigation: vision-based relative navigation and terrain-relative navigation.
  • Hazard avoidance: safe landing and proximity operations in uncertain environments.
  • On-board anomaly detection: detect faults early and reconfigure safely.

In simple terms: spacecraft increasingly handle “unexpected situations” without waiting for Earth.

Resources

  • NASA — mission profiles and GNC references.
  • MIT OCW — controls and estimation material.