Optimal reliability design for over-actuated systems based on the MIT rule: Application to an octocopter helicopter testbed-Reference-Cited by-同舟云学术

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Optimal reliability design for over-actuated systems based on the MIT rule: Application to an octocopter helicopter testbed

Published:2014-12 Issue: Volume:132 Page:196-206
ISSN:0951-8320
Container-title:Reliability Engineering & System Safety
language:en
Short-container-title:Reliability Engineering & System Safety

Author:

Chamseddine Abbas,Theilliol Didier,Sadeghzadeh Iman,Zhang Youmin,Weber Philippe

Publisher

Elsevier BV

Subject

Industrial and Manufacturing Engineering,Safety, Risk, Reliability and Quality

Reference24 articles.

1. Fault tolerant control using sliding modes with on-line control allocation;Alwi;Automatica,2008

2. Adaptive control;Astrom,2008

3. Beck RE. Application of control allocation methods to linear systems with four or more objectives [Ph.D. thesis]. Virginia Polytechnic Institute and State University; 2002.

4. Chamseddine A, Sadeghzadeh I, Zhang YM, Theilliol D, Khelassi A. Control allocation for a modified quadrotor helicopter based on reliability analysis. In: Proceedings of AIAA Infotech@Aerospace. Garden Grove, California, USA; 2012.

5. Regression models and life tables;Cox;J R Stat Soc,1972

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