Attitude update rate is one of the important indicators of star sensor performance. In order to resolve the problem of the low attitude update rate of star sensors, this paper proposes a star sensor attitude update method based on star point correction of rolling shutter exposure. Based on the characteristics of the asynchronous exposure of the rolling shutter, recursive estimation of the motion attitude and the corrected star point information were combined to realize multiple updates of the attitude in a single frame of the star map. Simulation and experimental results proved that the proposed method could increase the attitude update rate of a star sensor by 15 times, up to 150 Hz
Attitude estimation and angular velocity estimation are the most critical components of a spacecraft...
The paper focuses on the problem of determining high rate angular velocity directly from star-tracke...
A stellar gyroscope is a star based attitude propagator that is capable of propagating a spacecraft’...
Efficiency and reliability are key issues when a star sensor operates in tracking mode. In the case ...
The attitude accuracy of star sensors decreases rapidly when star images become motion-blurred under...
In this paper, a star tracker attitude estimation procedure with increased robustness and efficiency...
Under dynamic conditions, the centroiding accuracy of the motion-blurred star image decreases and th...
Star sensor is a preferred attitude measurement device for its extremely high accuracy. Star acquisi...
Under highly dynamic conditions, the star-spots on the image sensor of a star tracker move across ma...
The attitude accuracy of a star tracker decreases rapidly when star images become motion-blurred und...
This paper presents an original tracking algorithm designed for star trackers adopting CMOS sensing ...
This paper presents an original tracking algorithm designed for star trackers adopting CMOS sensing ...
This paper presents a novel attitude estimation algorithm for spacecraft using a star tracker. The a...
Due to the character of the original source materials and the nature of batch digitization, quality ...
This paper presents an innovative algorithm developed for attitude determination of a space platform...
Attitude estimation and angular velocity estimation are the most critical components of a spacecraft...
The paper focuses on the problem of determining high rate angular velocity directly from star-tracke...
A stellar gyroscope is a star based attitude propagator that is capable of propagating a spacecraft’...
Efficiency and reliability are key issues when a star sensor operates in tracking mode. In the case ...
The attitude accuracy of star sensors decreases rapidly when star images become motion-blurred under...
In this paper, a star tracker attitude estimation procedure with increased robustness and efficiency...
Under dynamic conditions, the centroiding accuracy of the motion-blurred star image decreases and th...
Star sensor is a preferred attitude measurement device for its extremely high accuracy. Star acquisi...
Under highly dynamic conditions, the star-spots on the image sensor of a star tracker move across ma...
The attitude accuracy of a star tracker decreases rapidly when star images become motion-blurred und...
This paper presents an original tracking algorithm designed for star trackers adopting CMOS sensing ...
This paper presents an original tracking algorithm designed for star trackers adopting CMOS sensing ...
This paper presents a novel attitude estimation algorithm for spacecraft using a star tracker. The a...
Due to the character of the original source materials and the nature of batch digitization, quality ...
This paper presents an innovative algorithm developed for attitude determination of a space platform...
Attitude estimation and angular velocity estimation are the most critical components of a spacecraft...
The paper focuses on the problem of determining high rate angular velocity directly from star-tracke...
A stellar gyroscope is a star based attitude propagator that is capable of propagating a spacecraft’...