Loading [a11y]/accessibility-menu.js
Attitude Tracking Control of Rigid Spacecraft With Actuator Misalignment and Fault | IEEE Journals & Magazine | IEEE Xplore

Attitude Tracking Control of Rigid Spacecraft With Actuator Misalignment and Fault


Abstract:

A control scheme is developed to address the attitude tracking problem of a rigid spacecraft. A sufficient condition to accommodate actuator misalignment is presented. Th...Show More

Abstract:

A control scheme is developed to address the attitude tracking problem of a rigid spacecraft. A sufficient condition to accommodate actuator misalignment is presented. The controller asymptotically stabilizes the closed-loop attitude tracking system. The desired attitude trajectories can be tracked in finite time, even in the presence of uncertain inertia tensor, external disturbances, actuator fault, and actuator misalignment. The attitude tracking performance of the controller is evaluated through an illustrative example.
Published in: IEEE Transactions on Control Systems Technology ( Volume: 21, Issue: 6, November 2013)
Page(s): 2360 - 2366
Date of Publication: 23 January 2013

ISSN Information:


References

References is not available for this document.