When faults of some flight actuators have occurred, the aggressive use of fault-free actuators is often caused. This study focuses on a fault-tolerant flight control (FTFC) scheme, which is capable of tolerating aircraft actuator failures and respecting the control authority of healthy actuators. Adaptive sliding mode control (ASMC) technique is exploited in the FTFC design to ensure that the amplitudes and rates of the healthy actuators remain within the limited ranges. Simulation studies of nonlinear Boeing 747 longitudinal model are carried out to validate the effectiveness of the proposed scheme.
The design of fault-tolerant flight control within actuator control authority
2016-08-01
6467795 byte
Conference paper
Electronic Resource
English
Design of an Actuator Fault Tolerant Flight Control System Using Fault Detection and Diagnosis
British Library Conference Proceedings | 2013
|Design of an Actuator Fault Tolerant Flight Control System Using Fault Detection and Diagnosis
SAE Technical Papers | 2013
|Framework for Simultaneous Sensor and Actuator Fault-Tolerant Flight Control
Online Contents | 2017
|