DocumentCode
2109364
Title
Application of commercial electronics in the motors and actuator systems for Mars surface missions
Author
Mojarradi, Mohammad M. ; Cozy, R. Scott ; Chen, Yuan ; Kolawa, Elizabeth A. ; Johnson, Michael ; Mccarthy, Thomas ; Levanas, Greg C. ; Blalock, Benjamin ; Burke, Gary ; Del Castillo, Linda ; Shapiro, Andrew A.
Author_Institution
Jet Propulsion Lab., California Inst. of Technol., Pasadena, CA, USA
Volume
4
fYear
2004
fDate
13-13 March 2004
Firstpage
2562
Abstract
Commercial-off-the-shelf electronic components (COTS) offer a very low cost and attractive solution for construction of electronic systems for Mars missions, including the actuator electronic systems for the Mars Rovers. One issue with using COTS lies in the difference between their specified operating temperature range (-55°C to125°C for military components) and the temperatures observed at the surface of Mars (-120°C to 20°C). To compensate for the difference between these temperatures, most of the electronics are placed in a central warm-electronics-box or WEB. In some cases, such as the distributed control system for the actuators, the electronic assemblies that are to be placed on or near the motors are outside of the central WEB. The experimental search consists of two steps. First, a short functional/non-functional test at -120°C is used to identify and narrow down the number of candidate COTS that can work at very cold temperatures. More extensive characterization of the parts that passes the short test is performed to determine the operating margins and estimate the thermal cycle life capability for the COTS parts. Finally, the operating margins of the COTS parts are published as a set of specifications.
Keywords
DC-DC power convertors; Mars; analogue-digital conversion; avionics; distributed control; electric actuators; electric motors; operational amplifiers; planetary rovers; planetary surfaces; power electronics; -120 to 20 degC; -55 to 125 degC; COTS; Mars Rovers; Mars surface missions; WEB; actuator electronic systems; central warm electronics box; commercial shelf electronic components; distributed control system; electronic assembly; functional-nonfunctional test; motors; thermal cycle life; Actuators; Assembly systems; Costs; Distributed control; Electronic components; Life estimation; Life testing; Mars; Performance evaluation; Temperature distribution;
fLanguage
English
Publisher
ieee
Conference_Titel
Aerospace Conference, 2004. Proceedings. 2004 IEEE
Conference_Location
Big Sky, MT
ISSN
1095-323X
Print_ISBN
0-7803-8155-6
Type
conf
DOI
10.1109/AERO.2004.1368050
Filename
1368050
Link To Document