This paper proposes a real-time fault-tolerant estimation approach for combined sensor fault
diagnosis and air data reconstruction. Due to simultaneous influence of winds and latent …

Several architectures exist to measure aerodynamic angles based on physical sensors. As
far as unmanned aerial vehicle (UAV) is concerned, traditional systems hardly comply with …

Unmanned Aerial Vehicles (UAV) design may involve issues on redundancy of the systems
due to restricted available space and allowable weight. Virtual sensors offer great …

Introduction of fly-by-wire and increasing levels of automation significantly improve the
safety of civil aircraft, and result in advanced capabilities for detecting, protecting and …

Redundancy requirements for UAV (Unmanned Aerial Vehicle) are hardly faced due to the
generally restricted amount of available space and allowable weight for the aircraft systems …

This paper addresses the selection and the monitoring of some key flight parameters along
with their estimation in nominal and degraded flight conditions including faulty sensors …

This paper investigates robust fault diagnosis of multiple air data sensor faults in the
presence of winds. The trade-off between robustness to winds and sensitivity to faults is …

This paper addresses the estimation of flight parameters in nominal and degraded flight
conditions when one or several specific sensors become faulty. Anticipating more stringent …

An integrated fault diagnosis based fault tolerant longitudinal control system architecture is
proposed for civil aircraft which can accommodate partial or total losses of angle of attack …

The development of an avionic system passes through several steps, which aim is to obtain
a reliable equipment able to confirm the initial theoretical design. All these steps can be …