International audienceThis paper introduces a new approach to the study of artificial equilibrium points in the circular restricted three-body problem for propulsion systems with continuous and purely radial thrust. The propulsion system is described by means of a general mathematical model that encompasses the behavior of different systems like a solar sail, a magnetic sail and an electric sail. The proposed model is based on the choice of a coefficient related to the propulsion type and a performance parameter that quantifies the system technological complexity. The propulsion system is therefore referred to as generalized sail. The existence of artificial equilibrium points for a generalized sail is investigated. It is shown that three d...
Propellantless propulsion systems allow innovative mission scenarios to be envisaged, including the ...
Propellantless propulsion systems allow innovative mission scenarios to be envisaged, including the ...
We consider periodic halo orbits about artificial equilibrium points (AEP) near to the Lagrange poin...
This paper proposes a new concept of creating artificial equilibrium points in the circular restrict...
Creating and maintaining Artificial Equilibrium Points (AEPs) in the restricted threebody problem is...
This Thesis presents a study of possible mission scenarios for spacecraft propelled by continuous-th...
The existence and dynamical properties of artificial equilibria for solar sails in the elliptical re...
This paper discusses the problem of maintaining an L1-type artificial equilibrium point in the Sun-[...
This paper discusses the problem of maintaining an L1-type artificial equilibrium point in the Sun-[...
This paper discusses the problem of maintaining an L1-type artificial equilibrium point in the Sun-[...
In this Note a new family of solar sail orbits will be investigated in the sun-Earth circular restri...
This paper proposes a new concept of creating artificial equilibrium points in the circular restrict...
This paper proposes a new concept of creating artificial equilibrium points in the circular restrict...
This paper proposes a new concept of creating artificial equilibrium points in the circular restrict...
The existence and dynamical properties of artificial equilibria for solar sails in the elliptical re...
Propellantless propulsion systems allow innovative mission scenarios to be envisaged, including the ...
Propellantless propulsion systems allow innovative mission scenarios to be envisaged, including the ...
We consider periodic halo orbits about artificial equilibrium points (AEP) near to the Lagrange poin...
This paper proposes a new concept of creating artificial equilibrium points in the circular restrict...
Creating and maintaining Artificial Equilibrium Points (AEPs) in the restricted threebody problem is...
This Thesis presents a study of possible mission scenarios for spacecraft propelled by continuous-th...
The existence and dynamical properties of artificial equilibria for solar sails in the elliptical re...
This paper discusses the problem of maintaining an L1-type artificial equilibrium point in the Sun-[...
This paper discusses the problem of maintaining an L1-type artificial equilibrium point in the Sun-[...
This paper discusses the problem of maintaining an L1-type artificial equilibrium point in the Sun-[...
In this Note a new family of solar sail orbits will be investigated in the sun-Earth circular restri...
This paper proposes a new concept of creating artificial equilibrium points in the circular restrict...
This paper proposes a new concept of creating artificial equilibrium points in the circular restrict...
This paper proposes a new concept of creating artificial equilibrium points in the circular restrict...
The existence and dynamical properties of artificial equilibria for solar sails in the elliptical re...
Propellantless propulsion systems allow innovative mission scenarios to be envisaged, including the ...
Propellantless propulsion systems allow innovative mission scenarios to be envisaged, including the ...
We consider periodic halo orbits about artificial equilibrium points (AEP) near to the Lagrange poin...