کد مقاله کد نشریه سال انتشار مقاله انگلیسی نسخه تمام متن
806752 1468238 2014 11 صفحه PDF دانلود رایگان
عنوان انگلیسی مقاله ISI
Optimal reliability design for over-actuated systems based on the MIT rule: Application to an octocopter helicopter testbed
موضوعات مرتبط
مهندسی و علوم پایه سایر رشته های مهندسی مهندسی مکانیک
پیش نمایش صفحه اول مقاله
Optimal reliability design for over-actuated systems based on the MIT rule: Application to an octocopter helicopter testbed
چکیده انگلیسی

This paper addresses the problem of optimal reliability in over-actuated systems. Overloading an actuator decreases its overall lifetime and reduces its average performance over a long time. Therefore, performance and reliability are two conflicting requirements. While appropriate reliability is related to average loads, good performance is related to fast response and sufficient loads generated by actuators. Actuator redundancy allows us to address both performance and reliability at the same time by properly allocating desired loads among redundant actuators. The main contribution of this paper is the on-line optimization of the overall plant reliability according to performance objective using an MIT (Massachusetts Institute of Technology) rule-based method. The effectiveness of the proposed method is illustrated through an experimental application to an octocopter helicopter testbed.

ناشر
Database: Elsevier - ScienceDirect (ساینس دایرکت)
Journal: Reliability Engineering & System Safety - Volume 132, December 2014, Pages 196–206
نویسندگان
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