Pre-launch testing of ATMS has characterized the principal calibration parameters and has enabled predictions of on-orbit performance with high levels of confidence. The prelaunch radiometric calibration of ATMS consists of using a Compact Antenna Test Range (CATR); thermal vacuum chamber; vibration testing; and electromagnetic and radio frequency interference testing. A more limited performance assessment of ATMS is planned during the spacecraft environmental testing.
Postlaunch calibration and validation consists of four phases: activation, functional evaluation and optimization, Intensive Cal/Val (ICV), and long-term monitoring. The ICV will end approximately 180 days after launch. This paper will describe the various calibration and validation tasks in the four phases and the team responsible. Some of the tasks include optimal space view selection; geolocation accuracy evaluation; RFI evaluation and mitigation; simultaneous nadir overpasses of other microwave sensors; on-orbit spacecraft maneuvers; simulation comparisons with radiosondes and numerical weather prediction models; and aircraft underflights.
We review an approach for on-orbit FOV calibration of the ATMS satellite instrument using vicarious calibration sources with high spatial frequency content (the Earth's limb, for example). The antenna beam is slowly swept across the target of interest and a constrained deconvolution approach is used to recover antenna pattern anomalies. The Earth's limb can also be exploited as an additional radiometric calibration source.