Abstract
Research into fault-tolerant control is a very actual problem and attracts many investigators. Their proposed solutions have fallen into two categories: passive and active. In the passive category, the impaired aircraft continues to operate with the same controller; the effectiveness of the scheme depends upon the original control law’s possessing a considerable degree of robustness. The active category involves either an on-line re-design of the control law after failure has occurred and has been detected, or the selection of a new pre-computed control law. In this chapter, the active methods are considered.
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Hajiyev, C., Caliskan, F. (2003). Flight Control Reconfiguration. In: Fault Diagnosis and Reconfiguration in Flight Control Systems. Cooperative Systems, vol 2. Springer, Boston, MA. https://doi.org/10.1007/978-1-4419-9166-9_10
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DOI: https://doi.org/10.1007/978-1-4419-9166-9_10
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