Electric Station Keeping of Geostationary Satellites: a Differential Inclusion Approach
The aim of this paper is to consider the modelling and control issues arising in the design of a station keeping system for geostationary satellites based on electric propulsion. In particular, a linear time-varying model for the dynamics of a geostationary satellite affected by perturbations is der...
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creator | Losa, D. Lovera, M. Drai, R. Dargent, T. Amalric, J. |
description | The aim of this paper is to consider the modelling and control issues arising in the design of a station keeping system for geostationary satellites based on electric propulsion. In particular, a linear time-varying model for the dynamics of a geostationary satellite affected by perturbations is derived and the longitude and latitude station keeping problem is then formulated as a constrained linear quadratic optimal control problem. A direct method based on the so-called differential inclusion approach is then proposed. Simulation results showing the feasibility of the control task on a spacecraft equipped with electric thrusters are also presented and discussed. |
doi_str_mv | 10.1109/CDC.2005.1583369 |
format | Conference Proceeding |
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In particular, a linear time-varying model for the dynamics of a geostationary satellite affected by perturbations is derived and the longitude and latitude station keeping problem is then formulated as a constrained linear quadratic optimal control problem. A direct method based on the so-called differential inclusion approach is then proposed. Simulation results showing the feasibility of the control task on a spacecraft equipped with electric thrusters are also presented and discussed.</description><identifier>ISSN: 0191-2216</identifier><identifier>ISBN: 9780780395671</identifier><identifier>ISBN: 0780395670</identifier><identifier>DOI: 10.1109/CDC.2005.1583369</identifier><language>eng</language><publisher>IEEE</publisher><subject>Automatic Control Engineering ; Chemicals ; Computer Science ; Earth ; Gravity ; Optimal control ; Physics ; Predictive models ; Propulsion ; Satellites ; Solar radiation ; Space Physics ; Space vehicles ; Vectors</subject><ispartof>44th IEEE Conference on Decision and Control, 2005 and 2005 European Control Conference. 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CDC-ECC '05</btitle><stitle>CDC</stitle><date>2005</date><risdate>2005</risdate><spage>7484</spage><epage>7489</epage><pages>7484-7489</pages><issn>0191-2216</issn><isbn>9780780395671</isbn><isbn>0780395670</isbn><abstract>The aim of this paper is to consider the modelling and control issues arising in the design of a station keeping system for geostationary satellites based on electric propulsion. In particular, a linear time-varying model for the dynamics of a geostationary satellite affected by perturbations is derived and the longitude and latitude station keeping problem is then formulated as a constrained linear quadratic optimal control problem. A direct method based on the so-called differential inclusion approach is then proposed. Simulation results showing the feasibility of the control task on a spacecraft equipped with electric thrusters are also presented and discussed.</abstract><pub>IEEE</pub><doi>10.1109/CDC.2005.1583369</doi><tpages>6</tpages></addata></record> |
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ispartof | 44th IEEE Conference on Decision and Control, 2005 and 2005 European Control Conference. CDC-ECC '05, 2005, p.7484-7489 |
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language | eng |
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source | IEEE Electronic Library (IEL) Conference Proceedings |
subjects | Automatic Control Engineering Chemicals Computer Science Earth Gravity Optimal control Physics Predictive models Propulsion Satellites Solar radiation Space Physics Space vehicles Vectors |
title | Electric Station Keeping of Geostationary Satellites: a Differential Inclusion Approach |
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