What is it about?
A sliding mode reconfigurable control algorithm is developed to deal with nonlinear aircraft system with partial or total loss of actuator faults.
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Why is it important?
A fault tolerant control without restructure the whole control system will enable more safety without high cost of redesign.
Perspectives
This method is proposed when effectiveness of the actuators are available through a FDA block.
Tao Wang
Read the Original
This page is a summary of: Sliding Mode Recon¯gurable Control with Application to Longitudinal Control of Boeing 747, August 2010, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/6.2010-7700.
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