CORE
🇺🇦
make metadata, not war
Services
Services overview
Explore all CORE services
Access to raw data
API
Dataset
FastSync
Content discovery
Recommender
Discovery
OAI identifiers
OAI Resolver
Managing content
Dashboard
Bespoke contracts
Consultancy services
Support us
Support us
Membership
Sponsorship
Community governance
Advisory Board
Board of supporters
Research network
About
About us
Our mission
Team
Blog
FAQs
Contact us
research
Fault tolerant sliding mode control design with piloted simulator evaluation
Authors
Halim Alwi
Christopher Edwards
J.A. Mulder
O. Stroosma
Publication date
4 June 2015
Publisher
'American Institute of Aeronautics and Astronautics (AIAA)'
Doi
Cite
Abstract
Copyright © 2008 American Institute of Aeronautics and AstronauticsThis paper considers sliding mode allocation schemes for fault tolerant control. The schemes allow redistribution of the control signals to the remaining functioning actuators when a fault or failure occurs. The paper analyzes the schemes and determines conditions under which closed–loop stability is retained for a certain class of faults and failures. It is shown that faults and even certain total actuator failures can be handled directly without reconfiguring the controller. The results obtained from implementing the controllers on the SIMONA research flight simulator, configured to represent a B747 aircraft, show good performance in both nominal and failure scenarios even in wind and gust conditions
Similar works
Full text
Open in the Core reader
Download PDF
Available Versions
Supporting member
Open Research Exeter
See this paper in CORE
Go to the repository landing page
Download from data provider
oai:ore.exeter.ac.uk:10871/173...
Last time updated on 03/08/2016