Fig. 6From: Dynamic precise orbit determination of Hayabusa2 using laser altimeter (LIDAR) and image tracking data setsa Residuals of LIDAR range of arc No. 3 in Table 1 (blue) and the corresponding computed range (red) after removing long-wavelength components via quadratic equation fitting. b The difference between the observed and computed ranges for arc No. 3. c The difference between observed and computed right ascension (blue) and declination (red) angles of the centroid directions viewed from the Hayabusa2 spacecraft for arc No. 3Back to article page