Spacecraft passive radiometry makes use of natural thermal emissions to remotely sense Earth phenomena of interest to science (surface moisture, for example) in microwave L-band where a terrestrial source thermal emission signal to space suffers less attenuation by the intervening atmosphere. Unfortunately, the relative insensitivity of the L-band region to atmospheric effects also makes it an extremely attractive spectral range for the wireless communications & radars that are causing radio frequency interference (RFI) with the spaceflight science radiometer instrument's terrestrial phenomenon signal of interest. Excision of just the RFI component from the composite signal is a tall challenge to the state-of-the-art technologies (that excise the entire sample where RFI is detected. The goals are: 1.1 Research and develop a unique Hilbert-Huang Transform Empirical Mode Decomposition Component for 2-Dimensions (HHT2 EMD2) functionality superseding each of the numerous state-of-the-art on-board and ground RFI detection and sample excision algorithms; 1.2 Develop the HHT2 based RFI Detection and Mitigation (HHT2-RFI-DM ) system - a unified RFI detection and RFI(t) component only excision groundbreaking technology.
Microwave active/passive radiometer is the premier instrument for remote sensing of Earth. However, it carries the price of non-linear response by its horn-receiver sensor and the radiometer operational frequency band of interest is overlapping with man-made radio-frequency interference sources (RFI). The state-of-the-art RFI detection and mitigation is paramount and it encompasses a variety of on-board instrumentation analog techniques, as well as on-board and ground digital data processing, employing dozens of RFI detection and mitigation computational algorithms (RFI-DM). For example, advanced algorithms for the Soil Moisture Active/Passive Mission (SMAP) microwave radiometer are run on the SMAP science data system ground support equipment which complements the on-board processing of sub-sampled bands and computation of data moments. For SMAP high-resolution mode of 3 km with a radiometric accuracy of 0.4 dB in order to meet the mission's science requirements, the RFI poses a significant error source for that measurement, as an interference-to-signal ratio of 10 dB may use the entire error budget. SMAP's RFI-DM is an integral part of its single radiometer instrument system and is using a two-fold RFI-DM strategy – on-board analog RF sub-channeling and on-board and ground RFI-DM computational techniques that detect and mitigate many RFI types. However, there remains an area of highly non-linear RFI noise not covered by these state-of-the-art. Furthermore, future Earth and planetary radiometers will carry arrays of receivers and require new technologies for RFI detection and mitigation. For example, the ESA's Earth Explorer soil moisture and ocean salinity (SMOS) mission payload instrument, Microwave Imaging Radiometer using Aperture Synthesis, consists of 69 individual radiometer receivers. By the means of interferometry the measurements from all the receivers are combined and an image from the target is obtained. The RFI-DM for radiometric images is in embryonic state. The task is to find significantly advanced miniaturized engineering solutions for the RFI-DM problem. The recently developed NASA Goddard technologies – the Hilbert-Huang Transform Real-Time Data Processing System (HHT-DPS-RT) for 1-D (HHT1) and 2-D (HHT2), can be further researched and developed for detecting and mitigating RFI noise in highly non-linear regions and for image radiometers. Research and development of a consolidated beyond-frontier reference RFI-DM HHT-based technology (RFI-DM-HHT) would simplify on-board RF signal processing and significantly improve efficiency and capability of RFI-DM on-board processing system. It will, as well, enhance ground systems data processing in RFI detection and mitigation domain by an order of magnitude and reduce the RFI-DM system overall cost. Our RFI-DM-HHT research and development goal is based on our recent research and development of the HHT1 and the HHT2 (IRAD-FY2010, IRAD-FY2011 – NASA patents pending) and will focus on two components: 1.1 We propose to research and develop the RFI-DM-HHT – a novel technology for spaceflight microwave radiometers' RFI noise detection and mitigation based on the Hilbert-Huang Transform Real-Time Data Processing System. This technology covers the state-of-the-art and allows an order of magnitude reduction in complexity of on-board analog signal sampling for separating RF signal into multiple bins, since HHT1 does it automatically in digital domain by extracting IMFs of different scales from the non-linear and non–stationary composite signal. FFT and other transforms for such work are not suitable since received RF signal is non-linear and non-stationary, for which the HHT has an advantageous ability. 1.2 The state-of-the-art is based on on-board sub-channeling and on the ground computation of "kurtosis" for pulsed RFI, thresholding, reference lookup tables and statistical analysis of raw count moments. The RFI-DM-HHT may deliver an effective natural decomposition of antenna signal into a specified number of IMFs instead of on-board RF analog hardware to filter signal into selected sub-bands, followed by extensive ground processing, as posted in 1.1. The RFI-DM-HHT will be further developed beyond the-sate-of-the-art to mitigate RFI sources not covered by the-state-of-the-art and mitigate new RFI sources. It will also be developed for RFI detection in image radiometers that is presently non-existent. These breakthrough RFI-DM-HHT technologies are all long-term new business return opportunities for GSFC and deliver significant enhancements in the RFI detection and mitigation domain.More »
This project benefits the Soil Moisture Active and Passive satellite mission (SMAP) radiometer instrument data analysis using the Hilbert-Huang Transform for 2-dimensions (HHT2 Empirical Mode Decomposition for 2D component) developed in this project.. It allows a novel way to detect Radi Frequency Interference (RFI) events and recover measurements contaminated by RFI events. This allows to recover some 10% data contaminated by RFI.More »
|Organizations Performing Work||Role||Type||Location|
|Goddard Space Flight Center (GSFC)||Lead Organization||NASA Center||Greenbelt, Maryland|
|Syneren Technologies Inc.||
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