This paper presents a fault-tolerant method for estimating the angular rate of uncontrolled bodies in space, such as failed spacecrafts. The bodies are assumed to be free of any sensors; however, a planned mission is assumed to track several features of the object by means of stereo-vision sensors. Tracking bodies in the space environment using these sensors is not, in general, an easy task: obtainable information regarding the attitude of the body is often corrupted or partial. The developed method exploits this partial information to completely recover the attitude of the body using a basis pursuit approach. An unscented Kalman filter can then be used to estimate the angular rate of the body
A star sensor based new method for estimation of satellite angular rates through derivative approach...
Abstract: The reconstruction technique is based on processing the measurements of two vect...
Copyright © 2017 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved...
This paper presents a fault-tolerant method for estimating the angular rate of uncontrolled bodies i...
One of the key functionalities required by an Active Debris Removal mission is the assessment of the...
A method for evaluating attitude and measuring angular rate of uncontrolled bodies in space, such as...
The knowledge of spacecrafts’ angular rate is required for attitude control and determination, gener...
This paper presents the results of a study to develop and evaluate an attitude and attitude rate est...
Abstract: Monitoring of quasi-steady accelerations onboard last spacecraft of theseries wa...
Abstract: We consider the reconstruction of spacecraft attitude motion by measurements of ...
Capturing and de-orbiting space debris for removal purpose is a manoeuvre that requires the assessme...
This work describes two algorithms for computing the angular rate and attitude in case of a gyro and...
Abstract: Monitoring of accelerations onboard previous spacecraft of the «Foton» series wa...
Spacecraft systems need increased on board autonomy to detect the occurred faults (e.g., faults in ...
A method is presented for fast estimation of the angular rate of a tumbling spacecraft in a low-Eart...
A star sensor based new method for estimation of satellite angular rates through derivative approach...
Abstract: The reconstruction technique is based on processing the measurements of two vect...
Copyright © 2017 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved...
This paper presents a fault-tolerant method for estimating the angular rate of uncontrolled bodies i...
One of the key functionalities required by an Active Debris Removal mission is the assessment of the...
A method for evaluating attitude and measuring angular rate of uncontrolled bodies in space, such as...
The knowledge of spacecrafts’ angular rate is required for attitude control and determination, gener...
This paper presents the results of a study to develop and evaluate an attitude and attitude rate est...
Abstract: Monitoring of quasi-steady accelerations onboard last spacecraft of theseries wa...
Abstract: We consider the reconstruction of spacecraft attitude motion by measurements of ...
Capturing and de-orbiting space debris for removal purpose is a manoeuvre that requires the assessme...
This work describes two algorithms for computing the angular rate and attitude in case of a gyro and...
Abstract: Monitoring of accelerations onboard previous spacecraft of the «Foton» series wa...
Spacecraft systems need increased on board autonomy to detect the occurred faults (e.g., faults in ...
A method is presented for fast estimation of the angular rate of a tumbling spacecraft in a low-Eart...
A star sensor based new method for estimation of satellite angular rates through derivative approach...
Abstract: The reconstruction technique is based on processing the measurements of two vect...
Copyright © 2017 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved...