We have carried out a geometric calibration of the CCD sensor of MICAS (Miniature Integrated Camera Spectrometer), a 4-inch aperture reflecting telescope on board the DS1 (Deep Space One) spacecraft, using laboratory data and in-flight images of star fields. The images suffer from significant distortion up to 4 pixels near the margins, an effect which we modelled by two-dimensional polynomials of 10th degree. The focal length of the camera is determined to be f = 686.55 +/- 0.05 mm, clearly above the nominal design value. In-flight images show that the geometric properties of the camera essentially have not changed. Following image geometric corrections on the basis of the laboratory data, positions of stars in the images can be predicted t...
We present a theoretical analysis of the Diffracto-Astrometry measuring algorithm. We generated Tiny...
The NASA Dawn spacecraft acquired thousands of images of asteroid Vesta during its year-long orbital...
Affected by the vibrations and thermal shocks during launch and the orbit penetration process, the g...
Satellite cameras are calibrated before launch in detail and in general, but it cannot be guaranteed...
This paper describes the geometric inflight calibration of the Modular Optoelectronic Multispectral ...
International audienceContext. For charge-coupled device (CCD) mosaic chips in the focal plane of a ...
Very high resolution optical satellites are imaging the object space by a combination of CCD-lines i...
Abstract—We describe a method that allows for accurate in-flight calibration of the interior orienta...
The accurate measurement of the position of celestial objects is a fundamental step for several astr...
A simple but effective approach is proposed for measuring the geometric distortion of a CCD field of...
Different cameras are used in space. From Russian film cameras over panoramic cameras up to digital ...
A simple but effective approach is proposed for measuring the geometric distortion of a CCD field of...
Small format, medium resolution CCD cameras are at present widely used for industrial metrology appl...
A precise astrometric calibration method is presented for a CCD image with a small field of view. It...
This study presents a series of cost-e_ective strategies for calibrating star trackers for microsate...
We present a theoretical analysis of the Diffracto-Astrometry measuring algorithm. We generated Tiny...
The NASA Dawn spacecraft acquired thousands of images of asteroid Vesta during its year-long orbital...
Affected by the vibrations and thermal shocks during launch and the orbit penetration process, the g...
Satellite cameras are calibrated before launch in detail and in general, but it cannot be guaranteed...
This paper describes the geometric inflight calibration of the Modular Optoelectronic Multispectral ...
International audienceContext. For charge-coupled device (CCD) mosaic chips in the focal plane of a ...
Very high resolution optical satellites are imaging the object space by a combination of CCD-lines i...
Abstract—We describe a method that allows for accurate in-flight calibration of the interior orienta...
The accurate measurement of the position of celestial objects is a fundamental step for several astr...
A simple but effective approach is proposed for measuring the geometric distortion of a CCD field of...
Different cameras are used in space. From Russian film cameras over panoramic cameras up to digital ...
A simple but effective approach is proposed for measuring the geometric distortion of a CCD field of...
Small format, medium resolution CCD cameras are at present widely used for industrial metrology appl...
A precise astrometric calibration method is presented for a CCD image with a small field of view. It...
This study presents a series of cost-e_ective strategies for calibrating star trackers for microsate...
We present a theoretical analysis of the Diffracto-Astrometry measuring algorithm. We generated Tiny...
The NASA Dawn spacecraft acquired thousands of images of asteroid Vesta during its year-long orbital...
Affected by the vibrations and thermal shocks during launch and the orbit penetration process, the g...