• DocumentCode
    391347
  • Title

    Optimal filtering in the presence of faulty measurement biases

  • Author

    Rapoport, Ilia ; Oshman, Yaakov

  • Author_Institution
    Dept. of Aerosp. Eng., Technion-Israel Inst. of Technol., Haifa, Israel
  • Volume
    2
  • fYear
    2002
  • fDate
    10-13 Dec. 2002
  • Firstpage
    2236
  • Abstract
    The problem of fault tolerant estimation with application to a system subjected to faulty measurement biases is addressed. A new estimation approach, called fault adaptive filtering, is proposed. The proposed estimation scheme consists of a single minimum variance state estimator, which takes into account fault probabilities, combined with a fault estimator, which provides estimates of these probabilities. Unlike the multiple model approach this method does not require a large number of parallel filters. On the other hand, unlike separate estimation and fault detection techniques, the fault adaptive filter is able to utilize partial information about the existence of faults. A numerical example of spacecraft attitude determination is presented, which demonstrates the performance of the proposed approach.
  • Keywords
    aerospace control; aircraft navigation; fault tolerance; parameter estimation; aerospace navigation; fault adaptive filter; fault adaptive filtering; fault detection; fault estimator; fault tolerant estimation; optimal filtering; spacecraft attitude determination; Adaptive filters; Fault detection; Fault tolerant systems; Filtering; Missiles; Navigation; Position measurement; Probability; Space vehicles; State estimation;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Decision and Control, 2002, Proceedings of the 41st IEEE Conference on
  • ISSN
    0191-2216
  • Print_ISBN
    0-7803-7516-5
  • Type

    conf

  • DOI
    10.1109/CDC.2002.1184864
  • Filename
    1184864