PublishedJournal Article© by Mirza Tariq Hamayun 2015. In this paper, integral sliding mode control ideas are combined with direct control allocation in order to create a fault tolerant control scheme. Traditional integral sliding mode control can directly handle actuator faults; however, it cannot do so with actuator failures. Therefore, a mechanism needs to be adopted to distribute the control effort amongst the remaining functioning actuators in cases of faults or failures, so that an acceptable level of closed-loop performance can be retained. This paper considers the possibility of introducing fault tolerance even if fault or failure information is not provided to the control strategy. To demonstrate the efficacy of the proposed scheme...
Operational failure of control surfaces is one of the main reasons leading to aircraft crash. Since ...
This paper develops a sliding mode fault tolerant control scheme based on a Linear Parameter Varying...
This is the author accepted manuscript. The final version is available from the publisher via the DO...
In this paper, integral sliding mode control ideas are combined with direct control allocation in or...
This is the author's version of an artiucle subseqiently published in IEEE Transactions on Automatic...
Copyright © 2013 Elsevier. NOTICE: this is the author’s version of a work that was accepted for pub...
Copyright © 2014 IEEE. Personal use of this material is permitted. Permission from IEEE must be obta...
Copyright © 2008 American Institute of Aeronautics and AstronauticsThis paper considers sliding mode...
Journal ArticleThis paper proposes an on-line sliding mode control allocation scheme for fault toler...
This is the author accepted manuscript. The final version is available from Wiley via the DOI in thi...
Journal ArticleThis paper presents a sliding-mode approach for fault-tolerant control of a civil air...
This is the author accepted manuscript. The final version is available from Elsevier via the DOI in ...
The key attribute of a Fault Tolerant Control (FTC) system is its ability to maintain overall system...
The thesis concerns the theoretical development and implemantation of sliding mode schemes for fault...
This is the author accepted manuscript. The final version is available from the publisher via the DO...
Operational failure of control surfaces is one of the main reasons leading to aircraft crash. Since ...
This paper develops a sliding mode fault tolerant control scheme based on a Linear Parameter Varying...
This is the author accepted manuscript. The final version is available from the publisher via the DO...
In this paper, integral sliding mode control ideas are combined with direct control allocation in or...
This is the author's version of an artiucle subseqiently published in IEEE Transactions on Automatic...
Copyright © 2013 Elsevier. NOTICE: this is the author’s version of a work that was accepted for pub...
Copyright © 2014 IEEE. Personal use of this material is permitted. Permission from IEEE must be obta...
Copyright © 2008 American Institute of Aeronautics and AstronauticsThis paper considers sliding mode...
Journal ArticleThis paper proposes an on-line sliding mode control allocation scheme for fault toler...
This is the author accepted manuscript. The final version is available from Wiley via the DOI in thi...
Journal ArticleThis paper presents a sliding-mode approach for fault-tolerant control of a civil air...
This is the author accepted manuscript. The final version is available from Elsevier via the DOI in ...
The key attribute of a Fault Tolerant Control (FTC) system is its ability to maintain overall system...
The thesis concerns the theoretical development and implemantation of sliding mode schemes for fault...
This is the author accepted manuscript. The final version is available from the publisher via the DO...
Operational failure of control surfaces is one of the main reasons leading to aircraft crash. Since ...
This paper develops a sliding mode fault tolerant control scheme based on a Linear Parameter Varying...
This is the author accepted manuscript. The final version is available from the publisher via the DO...