The TRIO smart sensor data acquisition system on a chip for space applications

Author

Kottaras, George ; Paschalidis, Nick ; Paschalidis, Vasilis

Author_Institution

Space Res. Lab., Democritus Univ. of Thrace, Xanthi, Greece

Volume

4

fYear

2004

fDate

6-13 March 2004

Firstpage

2384

Abstract

This paper presents several design and testing aspects of the TRIO smart sensor data acquisition chip, developed by JHU/APL for NASA spacecraft applications. TRIO includes a 10-bit self corrected ADC, 16/32 analog inputs, a front end multiplexer with selectable acquisition time, a current source, a memory unit, a serial and a parallel bus, and a control logic. So far TRIO is used in many missions including Contour, Messenger, Stereo, Pluto and the generic JPL X2000 spacecraft bus.

Keywords

analogue-digital conversion; constant current sources; data acquisition; integrated circuit testing; intelligent sensors; multiplexing equipment; space vehicle electronics; Contour spacecraft bus; Messenger spacecraft bus; NASA spacecraft application; Pluto spacecraft bus; Stereo spacecraft bus; TRIO data acquisition chip; analog inputs; control logic; current source; front end multiplexer; generic JPL X2000 spacecraft bus; memory unit; parallel bus; self corrected ADC; serial bus; smart sensor data acquisition system; Circuits; Data acquisition; Intelligent sensors; Multiplexing; NASA; Oscillators; Pluto; Space vehicles; System-on-a-chip; Temperature sensors;

fLanguage

English

Publisher

ieee

Conference_Titel

Aerospace Conference, 2004. Proceedings. 2004 IEEE

ISSN

1095-323X

Print_ISBN

0-7803-8155-6

Type

conf

DOI

10.1109/AERO.2004.1368033

Filename

1368033