Nanosatellite air bearing tests of fault-tolerant sliding-mode attitude control with unscented kalman filter

Mark Post; Junquan Li; Regina Lee

doi:10.2514/6.2012-5040

Nanosatellite air bearing tests of fault-tolerant sliding-mode attitude control with unscented kalman filter

Mark Post, Junquan Li, Regina Lee

Design, Manufacturing And Engineering Management

Research output: Contribution to conference › Paper › peer-review

11 Citations (Scopus)

259 Downloads (Pure)

Abstract

This paper documents the development and testing of a fault tolerant sliding mode attitude control algorithm for a nanosatellite with reaction wheel control actuation.

Original language	English
Number of pages	12
DOIs	https://doi.org/10.2514/6.2012-5040
Publication status	Published - 13 Aug 2012
Event	AIAA Guidance, Navigation, and Control Conference - Hyatt Regency, Minneapolis, United States Duration: 13 Aug 2012 → 16 Aug 2012

Conference

Conference	AIAA Guidance, Navigation, and Control Conference
Country/Territory	United States
City	Minneapolis
Period	13/08/12 → 16/08/12

Keywords

nanosatellite
air bearing tests
fault-tolerant
sliding mode attitude control
unscented Kalman filter

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10.2514/6.2012-5040

Post-etal-AIAA-GNCC-Nanosatellite-air-bearing-tests-of-fault-tolerant-sliding-mode-attitudeAccepted author manuscript, 1.85 MB

Cite this

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title = "Nanosatellite air bearing tests of fault-tolerant sliding-mode attitude control with unscented kalman filter",

abstract = "This paper documents the development and testing of a fault tolerant sliding mode attitude control algorithm for a nanosatellite with reaction wheel control actuation. ",

keywords = "nanosatellite, air bearing tests, fault-tolerant, sliding mode attitude control, unscented Kalman filter",

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AU - Post, Mark

AU - Li, Junquan

AU - Lee, Regina

PY - 2012/8/13

Y1 - 2012/8/13

N2 - This paper documents the development and testing of a fault tolerant sliding mode attitude control algorithm for a nanosatellite with reaction wheel control actuation.

AB - This paper documents the development and testing of a fault tolerant sliding mode attitude control algorithm for a nanosatellite with reaction wheel control actuation.

KW - nanosatellite

KW - air bearing tests

KW - fault-tolerant

KW - sliding mode attitude control

KW - unscented Kalman filter

UR - http://arc.aiaa.org/doi/pdf/10.2514/6.2012-5040

U2 - 10.2514/6.2012-5040

DO - 10.2514/6.2012-5040

M3 - Paper

T2 - AIAA Guidance, Navigation, and Control Conference

Y2 - 13 August 2012 through 16 August 2012

ER -

Nanosatellite air bearing tests of fault-tolerant sliding-mode attitude control with unscented kalman filter

Abstract

Conference

Keywords

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