AIAA Guidance, Navigation and Control Conference and Exhibit 2008
DOI: 10.2514/6.2008-7475
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Fault Detection for Deep Space Satellites

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Cited by 2 publications
(4 citation statements)
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“…Consider a deep-space satellite with 16 thrusters (organized in 4 sets), similar to the one presented by Williamson et al (2009) or Patton et al (2010). Its general shape is that of a cube with side length 2 m. Figure 1 summarizes the simulation of the closed-loop control of the satellite.…”
Section: Simulationmentioning
confidence: 99%
“…Consider a deep-space satellite with 16 thrusters (organized in 4 sets), similar to the one presented by Williamson et al (2009) or Patton et al (2010). Its general shape is that of a cube with side length 2 m. Figure 1 summarizes the simulation of the closed-loop control of the satellite.…”
Section: Simulationmentioning
confidence: 99%
“…There is also an emerging trend towards fully non-linear FDI methods [9, 10]. Using these methods, some authors have considered sensor faults only [7, 11–15], actuator faults only [9, 10, 16–20], or non-simultaneous sensor and actuator faults [8, 21, 22].…”
Section: Introductionmentioning
confidence: 99%
“…In aerospace, though, nonlinear models provide a more accurate representation of the vehicle complex behavior. Most of the methods have thus been extended via linearization [8]. There is also a emerging trend toward fully-nonlinear FDI methods [9,10].…”
Section: Introductionmentioning
confidence: 99%
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