Remote input/output (RIO) smart sensor analog-digital chip
First Claim
1. An integrated circuit for use in distributed data collection in a spacecraft comprising:
- a plurality of ports for receiving sensor signals, said ports being connected to a plurality of sensors in the spacecraft wherein at least one of said plurality of sensors is a temperature sensor wherein a temperature measurement does not require a voltage reference due to the presence of a low temperature coefficient resistor external to said integrated circuit;
a multiplexer having a plurality of inputs and an output, each of said ports being connected to one of said inputs of said multiplexer;
an analog-to-digital converter having an input and an output, said input of said analog-to-digital converter being connected to said output of said multiplexer, said analog-to-digital converter comprising a radiation-hardened comparator;
a radiation-hardened voltage reference connected to said analog-to-digital converter;
a memory connected to said output of said analog-to-digital converter; and
a serial bus connected to said memory.
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Accused Products
Abstract
An analog-digital, radiation-hardened, low-power Smart Sensor Data Acquisition and Control chip, specifically designed and developed for Spacecraft/Instrument Housekeeping and Controls. Sensor data (Temperatures, Voltages, Currents, Pressure, Digitals) are continuously measured, digitized, stored, and transmitted, and Control Actions (DACS, Timers, Digitals) are activated, through a standard bi-directional, digital serial bus (I2C). The chip also offers a Custom or Standard (like PCI) parallel bus interface for parallel readout internally communicating to the serial bus. The chip essentially eliminates spacecraft harness, and greatly simplifies system design.
62 Citations
14 Claims
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1. An integrated circuit for use in distributed data collection in a spacecraft comprising:
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a plurality of ports for receiving sensor signals, said ports being connected to a plurality of sensors in the spacecraft wherein at least one of said plurality of sensors is a temperature sensor wherein a temperature measurement does not require a voltage reference due to the presence of a low temperature coefficient resistor external to said integrated circuit;
a multiplexer having a plurality of inputs and an output, each of said ports being connected to one of said inputs of said multiplexer;
an analog-to-digital converter having an input and an output, said input of said analog-to-digital converter being connected to said output of said multiplexer, said analog-to-digital converter comprising a radiation-hardened comparator;
a radiation-hardened voltage reference connected to said analog-to-digital converter;
a memory connected to said output of said analog-to-digital converter; and
a serial bus connected to said memory. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12)
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13. An integrated circuit for use in distributed data collection in a spacecraft comprising a plurality of sensors, the integrated circuit comprising:
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a plurality of ports connected to said plurality of sensors in the spacecraft wherein at least one of said plurality of sensors is a temperature sensor wherein a temperature measurement does not require a voltage reference due to the presence of a low temperature coefficient resistor located external to said integrated circuit;
a multiplexer connected to each of said plurality of ports;
an analog-to-digital converter connected to said multiplexer;
a memory connected to said analog-to-digital converter; and
a serial bus connected to said memory. - View Dependent Claims (14)
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Specification