Northwestern Polytechnical University / Chinese

A Rad-Hard Mixed-Signal MCU for space applications

Updated:2021-07-31 20:05 Click:

Introduction

A radiation-hardened mixed-signal microcontroller system-on-chip (SoC) is required to construct a on-board computer built in fully-customized nanosatellites for space applications.

Architecture of the MCU

    In our proposed microcontroller, the processor design is based on open-source processor named openMSP430. The open source MSP430 core is a 16-bit RISC low-power processor that implements all the instruction sets of an MSP430x1xx family of MCUs. In order to enhance the reliability, a dual-modular redundant processor has been designed. The SRAM is mainly composed of storage arrays and peripheral circuits. The basic memory cell unit uses the 6T structure and optimizes the layout using the method in paper. To meet the above design requirements, an eight channels, 12bit, 2MS/s ADC is designe, and a 12-bit, 10MS/s DAC is designed. To provide the clock for all SoC modules, a 32/16/8/1MHz clock generator is designed. To complete the communication function, the I2C, SPI and UART interface buses are designed. Wi-Fi, ZigBee and S-Band communication modules can link to these buses.

Figure 1 The architecture of the proposed microcontroller SoC

Prototype chips and Experimental results

    The radiation-hardened microcontroller SoC is implemented with the 180nm CMOS process, named MSuC430V2. The microcontroller SoC’s micrograph is shown in Fig. 2. The 16-bit dual-modular redundant processor is located on the right side of the chip, the 1 kB SRAM memory is located at the top right of the chip, the ADC is located at the bottom left of the chip, the DAC is located at the left side of the chip, the clock generation is located at the center of the chip. The proposed SoC area of 5mm × 3mm. In order to test the function of the SoC, a customized mother-daughter PCB board is designed.

Figure 2 The micrograph of the proposed SoC

    The performance evaluation results are shown in Table 1. The proposed microcontroller SoC, namely MSuC430V2, could satisfy the requirements of satellites for ADR.

Table 1 Main specifications of the propsed SoC

Parameter

performance index

Process

TSMC 0.18μm,1.8/3.3V

Dynamic Power

1.9mW /   MHz

Area

4.5mm×5mm

CPU

16bits, 32MHz,   0.404 DMIPS/MHz

SRAM

8kB, 6T, Period   of memory access 30ns

ADC12

12bit,2MS/s,   10mW, 8 channel input

DAC12

12bit,   10MS/s,4mW

Oscillator

100KHz,1MHz,1MHz,   Jitter 1.41ns

PLL

32/16/8/1MHz,   Jitter 718ps

For more information, please readout the following paper.

 2019_MEJ_X.Ge_W.Gao.pdf

 

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