Electronics & Computers

Time-Multiplexed Pipelined FFT Implementation

Goddard Space Flight Center, Greenbelt, Maryland A fast Fourier transform (FFT) was developed as part of the Soil-Moisture Active/Passive (SMAP) project. The FFT was created on 16-bit data arriving at a rate of 48 MHz to run on a resource-constrained, space-grade field programmable gate array (FPGA).

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Method for Authorizing Critical Effector Commands in a Space-Based Integrated Modular Avionics System

Lyndon B. Johnson Space Center, Houston, Texas An Integrated Modular Avionics (IMA) architecture provides a common platform for software partitions with shared processing and input/output (I/O) resources. A key feature of the IMA architecture is I/O partitioning. An IMA system will prevent one software partition from changing an I/O resource that is owned by another software partition. This prevents one software partition from controlling the outputs of another due to hardware fault or software error. The IMA system must have protection mechanisms in place to enforce the I/O partitioning.

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Fully Configurable Interrupt Controller

The controller is used in a method for authorizing critical effector commands in a space-based integrated modular avionics system. Lyndon B. Johnson Space Center, Houston, Texas An interrupt is a signal in an interrupt controller (IC) that pulses to indicate an event or error. The IC is responsible for processing multiple internal interrupts and making these interrupts available to a host computer via a data bus or external output pins. Since there exist numerous interrupts, a method must be developed for routing the interrupts to the external output pins.

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Using a Multicast File Transfer Protocol to Update the Firmware of Multiple Embedded Devices Simultaneously

This method minimizes the amount of time and network bandwidth required to update the firmware in all smart sensor devices. John F. Kennedy Space Center, Florida Smart sensors for measuring temperature and pressure have been developed as part of the Advanced Ground Systems Maintenance (AGSM) project. The sensors have flash memory for storing firmware, calibration data, and configuration information. In anticipation of the sensors being installed at multiple locations (possibly numbering in the hundreds) around the Kennedy Space Center, a method was devised to update the firmware of many sensors quickly and easily.

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Model of Radiation Effects on Electronics (MREE)

Marshall Space Flight Center, Alabama An updated software model has been developed for predicting the single-event effect (SEE) rates in circuit designs as they are being designed. This tool will be used for estimating the frequency of the various SEEs, such as logic upsets and circuit latch-up. It may also be used to estimate the total radiation dose effects to microelectronic devices operated in the natural space radiation environment or in ionizing radiation test environments.

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COVE: A CubeSat Payload Processor

This processor is a reconfigurable FPGA-based electronics payload for advanced data processing applications. NASA’s Jet Propulsion Laboratory, Pasadena, California The COVE (CubeSat Onboard processing Validation Experiment) Payload Processor is JPL’s first on-orbit demonstration with the Xilinx Virtex-5 FPGA (field-programmable gate array). The electronics payload is designed to provide a platform for advanced data processing applications while conforming to CubeSat specifications. Measuring 9 × 9.5 × 2 cm, COVE carries the new radiation-hardened Virtex-5 FPGA (V5QV), magnetoresistive RAM (MRAM), and phase-change memory. All data access to/from the payload is facilitated through a shared memory interface via a direct serial peripheral interface (SPI). Multiple configuration options enable COVE to be reconfigured in flight with new FPGA firmware.

Posted in: Electronics & Computers, Briefs, TSP

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Dynamic Range Enhancement of High-Speed Data Acquisition Systems

Reversible non-linear amplitude compression is used. John H. Glenn Research Center, Cleveland, Ohio The innovation is a technique to overcome hardware limitations of common high-speed data acquisition systems in order to be able to measure electronic signals with high dynamic range, wide bandwidth, and high frequency.

Posted in: Electronics & Computers, Briefs, TSP

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