Papers

Peer-reviewed
Jan, 2018

Initial inflight calibration for Hayabusa2 optical navigation camera (ONC) for science observations of asteroid Ryugu

ICARUS
  • H. Suzuki
  • M. Yamada
  • T. Kouyama
  • E. Tatsumi
  • S. Kameda
  • R. Honda
  • H. Sawada
  • N. Ogawa
  • T. Morota
  • C. Honda
  • N. Sakatani
  • M. Hayakawa
  • Y. Yokota
  • Y. Yamamoto
  • S. Sugita
  • Display all

Volume
300
Number
First page
341
Last page
359
Language
English
Publishing type
Research paper (scientific journal)
DOI
10.1016/j.icarus.2017.09.11
Publisher
ACADEMIC PRESS INC ELSEVIER SCIENCE

Hayabusa2, the first sample return mission to a C-type asteroid was launched by the Japan Aerospace Exploration Agency (JAXA) on December 3, 2014 and will arrive at the asteroid in the middle of 2018 to collect samples from its surface, which may contain both hydrated minerals and organics. The optical navigation camera (ONC) system on board the Hayabusa2 consists of three individual framing CCD cameras, ONC-T for a telescopic nadir view, ONC-W1 for a wide-angle nadir view, and ONC-W2 for a wide-angle slant view will be used to observe the surface of Ryugu. The cameras will be used to measure the global asteroid shape, local morphologies, and visible spectroscopic properties. Thus, image data obtained by ONC will provide essential information to select landing (sampling) sites on the asteroid. This study reports the results of initial inflight calibration based on observations of Earth, Mars, Moon, and stars to verify and characterize the optical performance of the ONC, such as flat-field sensitivity, spectral sensitivity, point-spread function (PSF), distortion, and stray light of ONC-T, and distortion for ONC-W1 and W2. We found some potential problems that may influence our science observations. This includes changes in sensitivity of flat fields for all bands from those that were measured in the pre-flight calibration and existence of a stray light that arises under certain conditions of spacecraft attitude with respect to the sun. The countermeasures for these problems were evaluated by using data obtained during initial in-flight calibration. The results of our inflight calibration indicate that the error of spectroscopic measurements around 0.7 mu m using 0.55, 0.70, and 0.86 mu m bands of the ONC-T can be lower than 0.7% after these countermeasures and pixel binning. This result suggests that our ONC-T would be able to detect typical strength (similar to 3%) of the serpentine absorption band often found on CM chondrites and low albedo asteroids with >= 4 sigma confidence. (C) 2017 Elsevier Inc. All rights reserved.

Link information
DOI
https://doi.org/10.1016/j.icarus.2017.09.11
Web of Science
https://gateway.webofknowledge.com/gateway/Gateway.cgi?GWVersion=2&SrcAuth=JSTA_CEL&SrcApp=J_Gate_JST&DestLinkType=FullRecord&KeyUT=WOS:000414507300025&DestApp=WOS_CPL
ID information
  • DOI : 10.1016/j.icarus.2017.09.11
  • ISSN : 0019-1035
  • eISSN : 1090-2643
  • Web of Science ID : WOS:000414507300025

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