A method for evaluating attitude and measuring angular rate of uncontrolled bodies in space, such as space debris, has been developed. The measurement can be obtained by elaborating data coming from tracking few natural features of the objects. Tracking can be pursued for instance through a chaser spacecraft equipped with 3D-cameras. Continuous quaternion time series are obtained via compressed sensing (CS) techniques while a linear Kalman filter (KF) is used to estimate the angular rate. The developed method is robust to typical occlusions of cameras in space environment. © 2016 IEEE
In most spacecraft (SC) there is a need to know the SC angular rate. Precise angular rate is require...
Knowledge about the attitude state of space debris is necessary for the design of active debris remo...
A star sensor based new method for estimation of satellite angular rates through derivative approach...
A method for evaluating attitude and measuring angular rate of uncontrolled bodies in space, such as...
One of the key functionalities required by an Active Debris Removal mission is the assessment of the...
This paper presents a fault-tolerant method for estimating the angular rate of uncontrolled bodies i...
Capturing and de-orbiting space debris for removal purpose is a manoeuvre that requires the assessme...
The knowledge of spacecrafts’ angular rate is required for attitude control and determination, gener...
The structure of a space target, and estimates of its relative pose (position and orientation) and m...
Abstract – An architecture for the estimation of dynamic state, geometric shape, and model parameter...
Abstract: This paper presents an extended Kalman filter for real-time estimation of rigid body orie...
A new algorithm for estimating the angular velocity using quaternion measurements is developed base...
An algorithm with frame correlative detection and Kalman filtering tracking was proposed to detect t...
A method is presented for fast estimation of the angular rate of a tumbling spacecraft in a low-Eart...
Abstract: Monitoring of quasi-steady accelerations onboard last spacecraft of theseries wa...
In most spacecraft (SC) there is a need to know the SC angular rate. Precise angular rate is require...
Knowledge about the attitude state of space debris is necessary for the design of active debris remo...
A star sensor based new method for estimation of satellite angular rates through derivative approach...
A method for evaluating attitude and measuring angular rate of uncontrolled bodies in space, such as...
One of the key functionalities required by an Active Debris Removal mission is the assessment of the...
This paper presents a fault-tolerant method for estimating the angular rate of uncontrolled bodies i...
Capturing and de-orbiting space debris for removal purpose is a manoeuvre that requires the assessme...
The knowledge of spacecrafts’ angular rate is required for attitude control and determination, gener...
The structure of a space target, and estimates of its relative pose (position and orientation) and m...
Abstract – An architecture for the estimation of dynamic state, geometric shape, and model parameter...
Abstract: This paper presents an extended Kalman filter for real-time estimation of rigid body orie...
A new algorithm for estimating the angular velocity using quaternion measurements is developed base...
An algorithm with frame correlative detection and Kalman filtering tracking was proposed to detect t...
A method is presented for fast estimation of the angular rate of a tumbling spacecraft in a low-Eart...
Abstract: Monitoring of quasi-steady accelerations onboard last spacecraft of theseries wa...
In most spacecraft (SC) there is a need to know the SC angular rate. Precise angular rate is require...
Knowledge about the attitude state of space debris is necessary for the design of active debris remo...
A star sensor based new method for estimation of satellite angular rates through derivative approach...