The capability of an active spacecraft to accurately estimate its pose with respect to a target orbiting in close-proximity is required by activities like formation flying, on-orbit servicing, active debris removal, and space exploration. According to the specific mission scenario, pose determination involves theoretical and technological challenges related to the search for the most suitable algorithmic solution and sensor architecture. Electro-optical sensors represent the best technological option being compatible with mass and power limitations of micro and small satellites, and their measurements can be processed to estimate all the pose parameters. The degree of complexity of pose determination largely varies depending on the nature o...
The interest of the space community toward missions like On-Orbit Servicing of functional satellite ...
This paper presents an innovative approach to design relative trajectories suitable for close-proxim...
This paper deals with the problem of designing relative trajectories in Earth orbit between an activ...
The capability of an active spacecraft to accurately estimate its pose with respect to a target orbi...
This paper investigates the potential of multiple architectures for spacecraft pose determination re...
The relative pose estimation of an inactive target by an active servicer spacecraft is a critical ta...
Vision-based methods to determine the relative pose of an uncooperative orbiting object are investig...
The need to remove space junk from crowded orbital regimes has fostered the interest towards the dev...
In space attack and defense, on-orbital servicing, pose estimation of unknown (non-cooperative) spac...
Missions requiring autonomous, close-proximity operations of spacecraft, such as On-Orbit Servicing,...
In order to support spacecraft proximity operations, such as on-orbit servicing and spacecraft forma...
Close-proximity operations are increasingly a topic of interest, where satellites manoeuvre within a...
Non cooperative on-orbit operations, such as rendezvous, docking or berthing operations, have become...
This paper presents a concept and initial results of testing a vision system for satellite proximity...
A reliable method for estimating the pose of an unknown and uncooperative space target using monocul...
The interest of the space community toward missions like On-Orbit Servicing of functional satellite ...
This paper presents an innovative approach to design relative trajectories suitable for close-proxim...
This paper deals with the problem of designing relative trajectories in Earth orbit between an activ...
The capability of an active spacecraft to accurately estimate its pose with respect to a target orbi...
This paper investigates the potential of multiple architectures for spacecraft pose determination re...
The relative pose estimation of an inactive target by an active servicer spacecraft is a critical ta...
Vision-based methods to determine the relative pose of an uncooperative orbiting object are investig...
The need to remove space junk from crowded orbital regimes has fostered the interest towards the dev...
In space attack and defense, on-orbital servicing, pose estimation of unknown (non-cooperative) spac...
Missions requiring autonomous, close-proximity operations of spacecraft, such as On-Orbit Servicing,...
In order to support spacecraft proximity operations, such as on-orbit servicing and spacecraft forma...
Close-proximity operations are increasingly a topic of interest, where satellites manoeuvre within a...
Non cooperative on-orbit operations, such as rendezvous, docking or berthing operations, have become...
This paper presents a concept and initial results of testing a vision system for satellite proximity...
A reliable method for estimating the pose of an unknown and uncooperative space target using monocul...
The interest of the space community toward missions like On-Orbit Servicing of functional satellite ...
This paper presents an innovative approach to design relative trajectories suitable for close-proxim...
This paper deals with the problem of designing relative trajectories in Earth orbit between an activ...