All-Electric Spacecraft Precision Pointing Using Model Predictive Control
Author:
Affiliation:
1. Dipartimento di Ingegneria dell’Informazione e Scienze matematiche, Università di Siena, 53100 Siena, Italy
2. Aerospazio Tecnologie, Aerospazio Tecnologie s.r.l., Rapolano Terme, 53100 Siena, Italy
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Applied Mathematics,Electrical and Electronic Engineering,Space and Planetary Science,Aerospace Engineering,Control and Systems Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.G000347
Reference18 articles.
1. All-Electric Thruster Control of a Geostationary Communications Satellite
2. On-Orbit Testing of the EO-1 Pulsed Plasma Thruster
3. Electric Propulsion Subsystem Architecture for an All-Electric Spacecraft
4. Attitude controller design for a system using actuators with switching-time restrictions and delays
5. A signed switching time bang-bang attitude control law for fine pointing of flexible spacecraft†
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