2004 IEEE Aerospace Conference Proceedings (IEEE Cat. No.04TH8720)
DOI: 10.1109/aero.2004.1367683
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Real-time fault detection and situational awareness for rovers: report on the mars technology program task

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Cited by 57 publications
(32 citation statements)
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“…Thus f, D, v, a t and az can be updated and calculated by the observations generated in (23) and (4). The estimation errors of the parameters and states, calculated by (23) and (4) are shown from Figure 6 to Figure 10. The corresponding estimated mean errors are specified in Table 1.…”
Section: Simulation Resultsmentioning
confidence: 99%
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“…Thus f, D, v, a t and az can be updated and calculated by the observations generated in (23) and (4). The estimation errors of the parameters and states, calculated by (23) and (4) are shown from Figure 6 to Figure 10. The corresponding estimated mean errors are specified in Table 1.…”
Section: Simulation Resultsmentioning
confidence: 99%
“…These values are not calculated from (23). The values of parameter particles will be assigned from them.…”
Section: Simulation Resultsmentioning
confidence: 99%
See 1 more Smart Citation
“…Recently, computationally efficient approaches for approximating Bayesian belief using particle filters have been studied as a means for fault detection and identification (Dearden et al 2004;Verma et al 2004;Li and Kadirkamanathan 2001). Particle filters are Monte Carlo methods capable of tracking hybrid state spaces of continuous noisy sensor data and discrete operation states.…”
Section: Related Workmentioning
confidence: 99%
“…In these studies, banks of Kalman filters are applied to track multiple models with embedded fault states. Recently, computationally efficient approaches for approximating Bayesian belief using particle filters 1 have been suggested as a means for fault detection and identification [9,10,11].…”
Section: Related Workmentioning
confidence: 99%