International audienceThe problem of the computation of correction maneuvers for the fuel-optimal long-term station-keeping within a predefined longitude and latitude window of a geostationary satellite equipped with electric propulsion is investigated. The use of electric thrusters imposes some additional operational constraints on actuation that can be reformulated as logical constraints on the control function. The resulting fuel-optimal station-keeping problem is therefore transformed into a mixed linear integer programming problem. The long-term horizon of station-keeping is divided in shorter control cycles synchronized with the cycles of orbit determination, and the long-term station-keeping problem amounts to solve a sequence of sim...
The aim of the study is to determine the required maneuvers to control geostationary satellites with...
A method is developed to calculate station-keeping maneuvers for a fleet of satellites collocated in...
A method is developed to determine station-keeping maneuvers for a fleet of satellites collocated in...
International audienceThe problem of the computation of correction maneuvers for the fuel-optimal lo...
International audienceIn this paper, a control scheme is elaborated to perform the station keeping o...
International audienceIn this paper, a control scheme is elaborated to perform the station keeping o...
International audienceIn this paper, a control scheme is elaborated in order to perform the station ...
International audienceThe aim of this paper is to consider the modelling and control issues arising ...
Geostationary spacecraft have to stay above a fixed point of the Earth, on a so-called geostationary...
Pour mener à bien leur mission, les satellites de télécommunications doivent rester à la verticale d...
International audienceThe aim of this paper is to consider the modelling and control issues arising ...
International audienceThe optimal station keeping control problem of a geostationary satellite equip...
International audienceThe minimum fuel station keeping of a geostationary satellite equipped with el...
The generalized linear impulsive correction problem is applied to make a linear programming problem ...
This paper introduces a novel affine formulation of the equations of motion of a satellite in a geos...
The aim of the study is to determine the required maneuvers to control geostationary satellites with...
A method is developed to calculate station-keeping maneuvers for a fleet of satellites collocated in...
A method is developed to determine station-keeping maneuvers for a fleet of satellites collocated in...
International audienceThe problem of the computation of correction maneuvers for the fuel-optimal lo...
International audienceIn this paper, a control scheme is elaborated to perform the station keeping o...
International audienceIn this paper, a control scheme is elaborated to perform the station keeping o...
International audienceIn this paper, a control scheme is elaborated in order to perform the station ...
International audienceThe aim of this paper is to consider the modelling and control issues arising ...
Geostationary spacecraft have to stay above a fixed point of the Earth, on a so-called geostationary...
Pour mener à bien leur mission, les satellites de télécommunications doivent rester à la verticale d...
International audienceThe aim of this paper is to consider the modelling and control issues arising ...
International audienceThe optimal station keeping control problem of a geostationary satellite equip...
International audienceThe minimum fuel station keeping of a geostationary satellite equipped with el...
The generalized linear impulsive correction problem is applied to make a linear programming problem ...
This paper introduces a novel affine formulation of the equations of motion of a satellite in a geos...
The aim of the study is to determine the required maneuvers to control geostationary satellites with...
A method is developed to calculate station-keeping maneuvers for a fleet of satellites collocated in...
A method is developed to determine station-keeping maneuvers for a fleet of satellites collocated in...