• 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