Active Attitude Control Mechanisms

Nadjim Horri, Phil Palmer

Research output: Chapter in Book/Report/Conference proceedingEntry for encyclopedia/dictionary

Abstract

This section describes the fundamentals, operating principles, and dynamical modeling of the actuators used for active spacecraft attitude control. Magnetic torquers and thrusters are presented as a way of applying external control torques to a spacecraft to alter both attitude and momentum. Momentum exchange devices, consisting of reaction and momentum wheels and control moment gyros are then presented as means of generating internal control torques for the operational attitude control of a spacecraft. The evolution of space applications is putting increasingly stringent requirements on satellite attitude control performance, thence the increasing importance of attitude control hardware.
Original languageEnglish
Title of host publicationEncyclopedia of Aerospace Engineering
PublisherWiley
ISBN (Electronic)9780470686652
DOIs
Publication statusPublished - 15 Dec 2010

Keywords

  • actuators
  • magnetic torquer
  • thruster
  • reaction wheel
  • momentum wheel
  • control moment gyro

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  • Cite this

    Horri, N., & Palmer, P. (2010). Active Attitude Control Mechanisms. In Encyclopedia of Aerospace Engineering Wiley. https://doi.org/10.1002/9780470686652.eae299