Optical calibration of the DAWN framing cameras G. Abraham ,G. Kovacs, B. Nagy
Department of Mechatronics, Optics and Engineering Informatics Budapest University of Technology and Economics
Introduction
NASA has initiated the DAWN mission in the beginning of the new millennium.
The spacecraft shall be the first in the history of space research to visit two planetary bodies in one mission. The asteroid Vesta and the dwarf planet Ceres are both located in the asteroid belt between Mars and Jupiter. DAWN’s mission is to orbit these large “rocks” in space and gather as many data of them as possible. For this reason several instruments are placed upon the spacecraft such as framing cameras, gamma ray and neutron spectrometer and visible/infrared (VIR) spectrometer.
Fig.1. The DAWN spacecraft
The DAWN spacecraft has two redundant Framing Cameras (FC) on board for scientific imaging and navigation purposes. These functional eyes of the spacecraft will support spacecraft maneuvers, orbit insertion and maintenance at the target asteroids. For in-flight calibration, star fields, clusters, and solar system objects will be imaged.
Fig.2 The 3D modell of the DAWN cameras
To achieve high-resolution images the FC’s have a four lens telecentric optical design with filters for spectral band imaging (polychromatic ‘clear’ filter) and seven filters from the blue wavelengths up to the near infrared band and a CCD detector (Fig.2.) The flight units of Framing Cameras were calibrated at the Max Planck Institute for Solar System Research (MPS) in Lindau, Germany. The calibration campaign and image data analysis was supported by optical engineers from the Budapest University of Technology and Economics, Hungary.
Methods
The optical calibration of the FC focused on the imaging properties of the integrated device, including the lens system, baffle, filters, the CCD and the elec- tronics. Several combinations of CCD exposures and spectral bands were tested to gain as much information as possible on the resolution, contrast, homogeneity and irradiation properties. The measurements were carried out in four main categories.
Fig.3. DAWN framing camera in the vacuum chamber
PSF: the actual focal position and the image resolution was determined by the Point Spread Function (PSF) measurement.
MTF: The Modulation Transfer Function (MTF) measurement shows the contrast ratio of the FC. Different spatial resolutions on a USAF target were imaged by the optical system up to the CCD’s Nyquist frequency. The contrast values at the various spatial frequencies provided the modulation transfer function which had to be in line with the optical specifications.
RAD: The cameras spectral response and the whole system’s quantum efficiency
was determined by the RAD tests. The exit slit of a high resolution
monochromator was imaged by a collimator and the camera to the CCD.
FLAT: An integrating sphere was used to test the light energy distribution over the detectors surface homogeneously.
PSF
The goal of this test was to determine the PSF (point spread function) of the FC for all filters at certain specified field angles. The measurements were carried out by simulating different focal positions, so we could establish the best focus position of the camera for all filters. This was critical, because of the wide spectral range, and the method of chromatic correction, involving different filter thicknesses. (Fig.4.)
Fig.4. Modelling the PSF
A target with a 0.035 mm pinhole was positioned at the focus of a reflective collimator (F=1750mm) providing a 11.6X reduction on the image plane (Fig.5.) The target war translated along the optical axis, and several images were shot to find the minimum on- and off-axis spot. The measurement used sub-pixel camera movements to cope with the CCD aliasing effects.
Halogen lamp Condenser Pinhole Collimator
Rotator
Dawn FC