Real time fault tolerant nonlinear attitude control system for nanosatellite applications

Junquan Li, Mark Post, Regina Lee

Research output: Contribution to conferencePaper

Abstract

This paper develops a fault tolerant attitude controller for next generation nanostatellites.

Conference

ConferenceInfotech@Aerospace 2012
CountryUnited States
CityGarden Grove, California
Period19/06/1221/06/12
Internet address

Fingerprint

Nanosatellites
nanosatellites
attitude control
Attitude control
control system
controllers
Control systems
Controllers

Keywords

  • nonlinear attitude control system
  • nanosatellite applications
  • real time
  • fault tolerant

Cite this

Li, J., Post, M., & Lee, R. (2012). Real time fault tolerant nonlinear attitude control system for nanosatellite applications. Paper presented at Infotech@Aerospace 2012, Garden Grove, California, United States. https://doi.org/10.2514/6.2012-2428
Li, Junquan ; Post, Mark ; Lee, Regina. / Real time fault tolerant nonlinear attitude control system for nanosatellite applications. Paper presented at Infotech@Aerospace 2012, Garden Grove, California, United States.23 p.
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author = "Junquan Li and Mark Post and Regina Lee",
year = "2012",
month = "6",
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language = "English",
note = "Infotech@Aerospace 2012 ; Conference date: 19-06-2012 Through 21-06-2012",
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Li, J, Post, M & Lee, R 2012, 'Real time fault tolerant nonlinear attitude control system for nanosatellite applications' Paper presented at Infotech@Aerospace 2012, Garden Grove, California, United States, 19/06/12 - 21/06/12, . https://doi.org/10.2514/6.2012-2428

Real time fault tolerant nonlinear attitude control system for nanosatellite applications. / Li, Junquan; Post, Mark; Lee, Regina.

2012. Paper presented at Infotech@Aerospace 2012, Garden Grove, California, United States.

Research output: Contribution to conferencePaper

TY - CONF

T1 - Real time fault tolerant nonlinear attitude control system for nanosatellite applications

AU - Li, Junquan

AU - Post, Mark

AU - Lee, Regina

PY - 2012/6/19

Y1 - 2012/6/19

N2 - This paper develops a fault tolerant attitude controller for next generation nanostatellites.

AB - This paper develops a fault tolerant attitude controller for next generation nanostatellites.

KW - nonlinear attitude control system

KW - nanosatellite applications

KW - real time

KW - fault tolerant

UR - http://arc.aiaa.org/doi/abs/10.2514/6.2012-2428

UR - http://www.aiaa.org/EventDetail.aspx?id=4683

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DO - 10.2514/6.2012-2428

M3 - Paper

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Li J, Post M, Lee R. Real time fault tolerant nonlinear attitude control system for nanosatellite applications. 2012. Paper presented at Infotech@Aerospace 2012, Garden Grove, California, United States. https://doi.org/10.2514/6.2012-2428