Active fault tolerant control for vertical tail damaged aircraft with dissimilar redundant actuation system
نویسندگان
چکیده
منابع مشابه
Active Fault Tolerant Control for Vertical Tail Damaged Aircraft with Dissimilar Redundant Actuation System
This Article is brought to you for free and open access by the Engineering Technology at ODU Digital Commons. It has been accepted for inclusion in Engineering Technology Faculty Publications by an authorized administrator of ODU Digital Commons. For more information, please contact [email protected]. Repository Citation Jun, Wang; Shaoping, Wang; Xingjian, Wang; Cun, Shi; and Tomovic, Mil...
متن کاملFault Tolerant Control for Damaged Aircraft Based on Sliding Mode Control Scheme
In this paper, the problem of structural damage with partial loss vertical tail in aircraft dynamical system is investigated. A linearized aircraft model is introduced firstly, then a damage-tolerant controller based on an adaptive sliding mode control is proposed. Finally, simulations with an aircraft model are conducted to demonstrate the effectiveness and advantages of the proposed design te...
متن کاملA Fault Tolerant Voter Circuit for Triple Modular Redundant System
Defect rate in Nanoelectronics is much higher than conventional CMOS circuits. Hardware redundancy can be a suitable solution for fault tolerance in nano level. A voter circuit is a part of a redundancy based fault tolerant system that enables a system to continue operating properly in the event of one or more faults within its components. Robustness of the voter circuit defines the reliability...
متن کاملGuidance and Nonlinear Active Fault Tolerant Control for General Aviation Aircraft
This paper addresses the development of a novel Active Fault Tolerant Control Scheme (AFTCS) which, when used with an independently designed guidance system, turns out to give an overall fault tolerant guidance and control system. This AFTCS methodology avoids a logic-based switching controller by exploiting an adaptive fault estimator whose design is based on the Non Linear Geometric Approach ...
متن کاملذخیره در منابع من
با ذخیره ی این منبع در منابع من، دسترسی به آن را برای استفاده های بعدی آسان تر کنید
ژورنال
عنوان ژورنال: Chinese Journal of Aeronautics
سال: 2016
ISSN: 1000-9361
DOI: 10.1016/j.cja.2016.08.009