PDS_VERSION_ID = PDS3 RECORD_TYPE = STREAM OBJECT = TEXT NOTE = "Known errors and/or anomalies in the volumes" PUBLICATION_DATE = 2010-11-18 END_OBJECT = TEXT END ERRORS AND/OR ANOMALIES IN THE CURRENT VOLUME Volume CORADR_0207, Version 02 ------------------------------ 1. The Cassini Radar Transition file (EXTRAS/CRT_207_V02.TAB) contains no information about ScanStart and ScanEnd transitions. 2. The uncompressed LBDR and BIDR products have attached labels. Normally, a file that has been compressed with ZIP would have been generated without an attached label. 3. In the volume index table (INDEX/INDEX.TAB), double quotes enclose all the date/time values. Normally, PDS date/time values are not quoted, but quoting makes parsing easier for some applications. 4. The HTML documents in the DOCUMENT directory contain HTML character codes that, while all-ASCII, are not easily interpretable by someone who is reading the HTML documents as text documents. For example, "α" represents the lower-case Greek character "alpha" and is rendered as such in a web browser. Equivalent and more legible character codes (e.g., "&#alpha;") are available as of the HTML 4.0 specification but cannot be used here, as PDS requires HTML documents to comply to the HTML 3.2 specification. 5. Antenna temperature, brightness temperature, and receiver temperature are defined in Janssen, M. A., "An Introduction to the Passive Microwave Remote Sensing of Atmospheres," Chapter 1 in Atmospheric Remote Sensing by Microwave Radiometry, (M. Janssen, ed.), pp. 1-35, Wiley & Sons, New York (1993). The archived value in the SBDR and LBDR files gives uncalibrated antenna temperature in units of Kelvin. The best current algorithm for correcting the archived antenna temperatures is Ta_corrected = Ta_archive * ( 0.920 - 0.0041*( t - 1.90 ) ) where t = time in years and fractional years since 2004.0 (0 UTC on 1 Jan 2004) This algorithm is based on the radioastronomical flux scale at 2-cm wavelength by direct comparison of distant (unresolved) Titan measurements by the Cassini radiometer with VLA measurements of Titan reported by Butler and Gurwell, 2004. This algorithm will improve with time as more distant Titan measurements are obtained and as more radioastronomical comparison sources are included. Butler, B. J., Gurwell, M. A. 2004. Radio Wavelength Observations of Titan with the VLA. Bull. Am. Astron. Soc. 36, 6.04. This algorithm applies also to all preceeding volumes. 6. Ideally the calibrated antenna temperature is referenced to cold sky at 2.7 K, although no guarantee is made that this zero-level accounting has been correctly made. Also, the antenna temperature is defined for this application as just the average brightness temperature in the measured beam out to 2 degrees from the beam axis, and does not allow for possible contributions from the far sidelobes (sidelobes outside of 2 degreees). The archived value will include an additional contribution if the far sidelobes happen to fall on other than cold sky. In particular, there is an offset to be expected and accounted for when an extended source like Titan or Saturn is observed from a close distance. A more detailed explanation will be found in Janssen et al., 2009. System gain is the quantity that multiplies the raw sky counts to convert to the uncalibrated Kelvin scale. Receiver_temp is the receiver noise temperature Tr (comparison made at internal reference switch). The receiver temperature plus the antenna temperature is equal to the total signal (raw counts times system gain). 7. ant_temp_std is a measure of the rms uncertainty of Ta, and is only an estimation. It is obtained as the standard deviation of Ta for three points, Ta(I-1), Ta(I), and Ta(I+1), and is a useful measure that identifies questionable data. For example, it gets large when the beam is sweeping across a brightness discontinuity. 8. All BIDRs except for the byte-valued backscatter images (BIB*.IMG) were produced by JPL. The byte-valued backscatter images were produced by USGS. The USGS BIDRs have unit strings in their labels which are all CAPS. The other BIDRs have lower case units. According to the PDS dictionary, both are acceptable. 9. Checksums were not computed for floating point valued BIDRs. The CHECKSUM keyword was assigned a zero value. 10. Typically SAR observations are only obtained for Titan. The Enceladus observation contained in this volume is one of only a handful of non-Titan Cassini SAR observations. As such, there are some differences in the data from nominal Titan SAR observations. The remainder of the list describes those differences. 11. The "noise subtraction" technique applied to remove systematic biases due to thermal noise and other effects differs form that used for Titan SAR observations. Because the geometry of this observation is at extremely long range and Enceladus is much smaller than Titan, the shape of the return echo in range and Doppler space differs dramatically from nominal Titan SAR data. The empirical model of the distortion of the signal due to downlink compression is not valid for this observation.For this reason only thermal noise subtraction was performed. An estimate of the thermal noise in each pixel due to 842 K of system noise temperature was subtracted from the images. The chosen noise temperature included 809 K due to the instrument and 33 K due to emission from Enceladus's surface.Errors in this approach lead to negative backscatter measurements for pixels at extremely large (> 60 degree) incidence angles. 12. In order to estimate the normalized backscatter cross-section from the returned echo power in each SAR pixel it is necessary to divide by the integral of the two-way antenna gain divided by the range to the fourth power. This integral is performed over the area on the surface of Enceladus for each SAR pixel. For nominal Titan SAR, pixels are small compared to the gain pattern and rectangularly-shaped so that a simple approximation can be used without resorting to a full numerical integration. For Enceladus the full integration was performed for each pixel with a 500 m step size. 13. Geolocation on the surface of Iapetus makes use of the nominal triaxial shape of Enceladus (radx,rady,radz)=(256.6,251.4,248.3) km rather than assuming a sphere as was done for Titan. Nonethless in order to simplify the map projection the images were projected onto a 252.1233 km radius sphere as described in the labels for each BIDR file. These coordinates are not the same as the planetodetic coordinates reported in the LBDR and SBDR files. 14. The correction used to remove incidence angle variation in the BIF*.IMG and BIU*.IMG files was different than that used for Titan. Each pixel was multiplied by a function of incidence angle f(I)=2.9165/(3.71*cos(I)^1.46) 15. Because of the extreme range (32,000 km) of the SAR observation in this volume and high relative velocity (8 km/s), the geolocation code was modified to account for the effect of special relativity on Doppler shift. Without this change, the geolocation would have been in error by 1.5 pixels. This error corresponds to 3 parts in one hundred thousand of the overall Doppler shift of the echo. Such a high level of fidelity was not needed for previous volumes in which the geo-location error due to relativity was much less than a pixel width. 16. Because the nadir point is close to the top of the SAR images, pixels near the top of the images are elongated and may contain significant energy from the mirror (identical range and Doppler) regions on the other side of the nadir point. These pixels have been calibrated to account for their full extent on the surface including the regions on both sides of nadir. Other pixels with significant ambiguous SAR energy were excluded. Mirror ambiguities were allowed because they are limited to the low resolution region at the top of the image and the backscatter values near nadir may be useful for scientific purposes despite the ambiguity in their locations. 16. The act_incidence_angle parameter in the SBDR and LBDR was redefined to be consistent with the incidence angle used to compute the incidence angle corrected sigma0. The boresight incidence angle value normally reported does not represent the wide range of incidence angles observed within the antenna footprint. Instead, an effective incidence angle is reported that is a weighted average of the incidence angles observed. It is weighted by the estimated distribution of the return energy over incidence angle. 17. The three different imaging segments comprise data taken at slightly different times during Cassini's approach to Enceladus. ERRORS AND/OR ANOMALIES IN PREVIOUS VOLUMES Not Applicable