Active Incremental Nonlinear Dynamic Inversion for Sensor and Actuator Fault-Tolerant Control

This publication has 32 references indexed in Scilit:

• Performance comparison of representative model-based fault reconstruction algorithms for aircraft sensor fault detection and diagnosis
  Aerospace Science and Technology, 2020
• Flight path reconstruction – A comparison of nonlinear Kalman filter and smoother algorithms
  Aerospace Science and Technology, 2011
• Non-linear aircraft flight path reconstruction review and new advances
  Progress in Aerospace Sciences, 1999
• Robust exact differentiation via sliding mode technique
  Automatica, 1998
• Optimal two-stage Kalman filter in the presence of random bias
  Automatica, 1997
• Extension of Friedland's separate-bias estimation to randomly time-varying bias of nonlinear systems
  IEEE Transactions on Automatic Control, 1993
• Estimation of aircraft aerodynamic parameters from flight data
  Progress in Aerospace Sciences, 1989
• A separated bias identification and state estimation algorithm for nonlinear systems
  Automatica, 1983
• Implementation of self-tuning regulators with variable forgetting factors
  Automatica, 1981
• The invariance conditions in variable structure systems
  Automatica, 1969