About: Fault diagnosis scheme for nonlinear stochastic systems with time-varying fault: application to the rigid spacecraft control     Goto   Sponge   NotDistinct   Permalink

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  • This paper studies the problem of the fault estimation for a class of time-varying faults using output probability density function (PDF). In particular, the spacecraft control system is studied. First, the attitude control of the nonlinear model with uncertainties is given. Then, the measured output is viewed as a stochastic process and its PDF is modeled, which leads to a deterministic dynamical model including nonlinearities and uncertainties. A new adaptive fault diagnosis algorithm is proposed to improve the performance of the fault estimation.The proposed algorithm contains both the proportional and the integral term. The proportional term can improve the speed of the fault estimation, while the integral term can eliminate estimation error. Then, based on the linear matrix inequality (LMI) technique, a feasible algorithm is explored to find the designed parameters.Finally, simulation results of the spacecraftare given to show the efficiency of the proposed approach.
  • This paper studies the problem of the fault estimation for a class of time-varying faults using output probability density function (PDF). In particular, the spacecraft control system is studied. First, the attitude control of the nonlinear model with uncertainties is given. Then, the measured output is viewed as a stochastic process and its PDF is modeled, which leads to a deterministic dynamical model including nonlinearities and uncertainties. A new adaptive fault diagnosis algorithm is proposed to improve the performance of the fault estimation.The proposed algorithm contains both the proportional and the integral term. The proportional term can improve the speed of the fault estimation, while the integral term can eliminate estimation error. Then, based on the linear matrix inequality (LMI) technique, a feasible algorithm is explored to find the designed parameters.Finally, simulation results of the spacecraftare given to show the efficiency of the proposed approach. (en)
Title
  • Fault diagnosis scheme for nonlinear stochastic systems with time-varying fault: application to the rigid spacecraft control
  • Fault diagnosis scheme for nonlinear stochastic systems with time-varying fault: application to the rigid spacecraft control (en)
skos:prefLabel
  • Fault diagnosis scheme for nonlinear stochastic systems with time-varying fault: application to the rigid spacecraft control
  • Fault diagnosis scheme for nonlinear stochastic systems with time-varying fault: application to the rigid spacecraft control (en)
skos:notation
  • RIV/68407700:21230/12:00197378!RIV13-MSM-21230___
http://linked.open...avai/predkladatel
http://linked.open...avai/riv/aktivita
http://linked.open...avai/riv/aktivity
  • I, P(GAP103/12/1794), S
http://linked.open...iv/cisloPeriodika
  • 3
http://linked.open...vai/riv/dodaniDat
http://linked.open...aciTvurceVysledku
http://linked.open.../riv/druhVysledku
http://linked.open...iv/duvernostUdaju
http://linked.open...titaPredkladatele
http://linked.open...dnocenehoVysledku
  • 136258
http://linked.open...ai/riv/idVysledku
  • RIV/68407700:21230/12:00197378
http://linked.open...riv/jazykVysledku
http://linked.open.../riv/klicovaSlova
  • Attitude control; adaptive fault estimation; LMI; PDF (en)
http://linked.open.../riv/klicoveSlovo
http://linked.open...odStatuVydavatele
  • RU - Ruská federace
http://linked.open...ontrolniKodProRIV
  • [3C8DE7B630FD]
http://linked.open...i/riv/nazevZdroje
  • Cybernetics and Physics
http://linked.open...in/vavai/riv/obor
http://linked.open...ichTvurcuVysledku
http://linked.open...cetTvurcuVysledku
http://linked.open...vavai/riv/projekt
http://linked.open...UplatneniVysledku
http://linked.open...v/svazekPeriodika
  • 1
http://linked.open...iv/tvurceVysledku
  • Čelikovský, Sergej
  • Nguyen Hong, Quang
issn
  • 2223-7038
number of pages
http://localhost/t...ganizacniJednotka
  • 21230
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