Add to ORKGControl of spacecraft formations around lagrangian points, particularly L2 point of the Sun-Earth system. Classification of keywords and properties of formation paradigm are analysed, then dynamics are developed in the circular restricted three-body problem. Formation adopt leader-follower paradigm with the leader is positioned on a Lissajous orbit around L2 point. State-dependent Riccati equation control is applied on the nonlinear dynamics including Moon's gravitational perturbation and solar radiation pressure disturbance. Manoeuvres reported in simulations are relative the New Worlds Observer mission set to launch in 2020
The libration point orbits in the Sun-Earth/Moon system are formed by concurrent gravitational influ...
Paper given at Dynamics and Control of Systems and Structures in Space (DCSSS), 6th conference, Ri...
In this thesis we consider the problem of developing distributed control strategies for spacecraft f...
The use of the state-dependent Riccati equation (SDRE) technique for formation flying control in the...
Spacecraft formations possess many applications in the future of space exploration. During the last ...
In this paper, we present a method for trajectory generation and adaptive full-state feedback contro...
The aim of this paper is to propose a distributed control architecture for a solar sail-based format...
Space based observatory and interferometry missions, such as Terrestrial Planet Finder (TPF), Stella...
Multi-spacecraft formations, evolving near the vicinity of the libration points of the Sun-Earth/Moo...
An expanding interest in mission design strategies that exploit libration point regions demands the ...
A periodic halo orbit which exists about the interior Lagrange point for the Earth-sun system was de...
Previous studies for small formation flying dynamics about triangular libration points have determin...
In this thesis, several control techniques are applied to an occulter satellite for a given formatio...
In a quest to improve space-based observational ca-pability, an increasing number of investigators a...
A new control technique for deep-space spacecraft formation flying is proposed in this paper. The ci...
The libration point orbits in the Sun-Earth/Moon system are formed by concurrent gravitational influ...
Paper given at Dynamics and Control of Systems and Structures in Space (DCSSS), 6th conference, Ri...
In this thesis we consider the problem of developing distributed control strategies for spacecraft f...
The use of the state-dependent Riccati equation (SDRE) technique for formation flying control in the...
Spacecraft formations possess many applications in the future of space exploration. During the last ...
In this paper, we present a method for trajectory generation and adaptive full-state feedback contro...
The aim of this paper is to propose a distributed control architecture for a solar sail-based format...
Space based observatory and interferometry missions, such as Terrestrial Planet Finder (TPF), Stella...
Multi-spacecraft formations, evolving near the vicinity of the libration points of the Sun-Earth/Moo...
An expanding interest in mission design strategies that exploit libration point regions demands the ...
A periodic halo orbit which exists about the interior Lagrange point for the Earth-sun system was de...
Previous studies for small formation flying dynamics about triangular libration points have determin...
In this thesis, several control techniques are applied to an occulter satellite for a given formatio...
In a quest to improve space-based observational ca-pability, an increasing number of investigators a...
A new control technique for deep-space spacecraft formation flying is proposed in this paper. The ci...
The libration point orbits in the Sun-Earth/Moon system are formed by concurrent gravitational influ...
Paper given at Dynamics and Control of Systems and Structures in Space (DCSSS), 6th conference, Ri...
In this thesis we consider the problem of developing distributed control strategies for spacecraft f...