This paper addresses the problem of star identification in the presence of high slew rates, false objects and image deformations introduced by the rolling shutter. These problems can affect the operating life of star trackers and worsen the nominal performances. The proposed methodology relies on a technique named Improved Multi-Poles Algorithm, especially designed for robustness to false objects and slew rates. Angular velocities up to five degrees per second are considered so that stars are seen no more as near-circular spots but appear as streaks. The image deformation due to the rolling shutter of modern active pixel sensor detectors is compensated by means of a mathematical model based on a first order approximation of problem. A star ...
Optical rate sensors, in particular CCD arrays, will be used on Space Station Freedom to track stars...
Attitude estimation and angular velocity estimation are the most critical components of a spacecraft...
This dissertation addresses novel techniques in determining gyroless micro-satellite attitude and at...
The paper focuses on the problem of determining high rate angular velocity directly from star-tracke...
This work proposes a novel technique for the star pattern recognition for the Lost in Space, named M...
The paper focuses on the problem of determining high rate angular velocity based on star-tracker mea...
The performance of a star tracker is largely based on the availability of its attitude solution. Sev...
Star trackers are usually considered to be the most accurate sensors, able to achieve a sub-arcminut...
A star tracker provides the most accurate attitude solution in terms of arc seconds compared to the ...
Developing an autonomous and reliable attitude determination system is one of the most crucial requi...
Star-tracker systems are typically limited by the angular rates at which they operate due to the ten...
This paper presents an application for modern star trackers aimed at the estimation of the spacecraf...
The knowledge of spacecrafts’ angular rate is required for attitude control and determination, gener...
This paper deals with a fast and efficient Lost in Space algorithm for stars pattern recognition in ...
In the previous study, there were a few direct star identification (star-ID) algorithms for smearing...
Optical rate sensors, in particular CCD arrays, will be used on Space Station Freedom to track stars...
Attitude estimation and angular velocity estimation are the most critical components of a spacecraft...
This dissertation addresses novel techniques in determining gyroless micro-satellite attitude and at...
The paper focuses on the problem of determining high rate angular velocity directly from star-tracke...
This work proposes a novel technique for the star pattern recognition for the Lost in Space, named M...
The paper focuses on the problem of determining high rate angular velocity based on star-tracker mea...
The performance of a star tracker is largely based on the availability of its attitude solution. Sev...
Star trackers are usually considered to be the most accurate sensors, able to achieve a sub-arcminut...
A star tracker provides the most accurate attitude solution in terms of arc seconds compared to the ...
Developing an autonomous and reliable attitude determination system is one of the most crucial requi...
Star-tracker systems are typically limited by the angular rates at which they operate due to the ten...
This paper presents an application for modern star trackers aimed at the estimation of the spacecraf...
The knowledge of spacecrafts’ angular rate is required for attitude control and determination, gener...
This paper deals with a fast and efficient Lost in Space algorithm for stars pattern recognition in ...
In the previous study, there were a few direct star identification (star-ID) algorithms for smearing...
Optical rate sensors, in particular CCD arrays, will be used on Space Station Freedom to track stars...
Attitude estimation and angular velocity estimation are the most critical components of a spacecraft...
This dissertation addresses novel techniques in determining gyroless micro-satellite attitude and at...