Feedback linearization-based satellite attitude control with a life-support device without communications. Giuseppi, A., Pietrabissa, A., Cilione, S., & Galvagni, L. Control Engineering Practice, 90:221-230, 2019. doi abstract bibtex This paper develops a control strategy for a life-support device to be attached to an orbiting satellite to extend its operational life. The objective is met in such a way that the original satellite keeps operating without communications between the two systems (also valuable for energy efficiency). The case in which the original satellite is equipped with a feedback-linearization based controller is considered and the control law for the life-support is developed with the same methodology, obtaining a compensating control which recovers the performance of the original control strategy. Simulations validate the approach considering a real case study in various scenarios. © 2019 Elsevier Ltd
@ARTICLE{Giuseppi2019221,
author={Giuseppi, A. and Pietrabissa, A. and Cilione, S. and Galvagni, L.},
title={Feedback linearization-based satellite attitude control with a life-support device without communications},
journal={Control Engineering Practice},
year={2019},
volume={90},
pages={221-230},
doi={10.1016/j.conengprac.2019.06.020},
scopus={https://www.scopus.com/inward/record.uri?eid=2-s2.0-85068760811&doi=10.1016%2fj.conengprac.2019.06.020&partnerID=40&md5=597bbced6acb84d3a68b7ab8c184926f},
abstract={This paper develops a control strategy for a life-support device to be attached to an orbiting satellite to extend its operational life. The objective is met in such a way that the original satellite keeps operating without communications between the two systems (also valuable for energy efficiency). The case in which the original satellite is equipped with a feedback-linearization based controller is considered and the control law for the life-support is developed with the same methodology, obtaining a compensating control which recovers the performance of the original control strategy. Simulations validate the approach considering a real case study in various scenarios. © 2019 Elsevier Ltd},
author_keywords={Feedback linearization; Model predictive control; Satellite systems; Spacecraft attitude control},
keywords={Artificial life; Attitude control; Control theory; Energy efficiency; Model predictive control; Orbits; Satellites; Space flight, Compensating control; Control strategies; Life supports; Operational life; Orbiting satellites; Satellite attitude control; Satellite system; Spacecraft attitude control, Feedback linearization},
document_type={Article},
source={Scopus},
}
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