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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Hauptverfasser: Losa, D., Lovera, M., Drai, R., Dargent, T., Amalric, J.
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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.
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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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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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