Periodic attitude control techniques for small satellites with magnetic actuators

2002171 citationsJournal Article

Authors

Eliana De Marchi · Politecnico di Milano

S. Bittanti · Venezia Tecnologie (Italy)

Abstract

The problems of attitude stabilization and disturbance torque attenuation for a small spacecraft using magnetic actuators is considered and a solution to the problem in terms of optimal periodic control is proposed, based on an optimal estimation and compensation scheme for external disturbances for linear time-periodic systems.

Topics & Keywords

Inertial Sensor and Navigation Aerospace Engineering and Control Systems Adaptive Control of Nonlinear Systems

UN Sustainable Development Goals

Affordable and clean energy

Publication Details

Published in: IEEE Transactions on Control Systems Technology

Volume 10, Issue 1, pp. 90-95

DOI: 10.1109/87.974341

Field-Weighted Citation Impact: 15.06