Reliable Control Optimization in Aerospace Engineering at Stochastic Stream of Faults
نویسندگان
چکیده
منابع مشابه
Design search and optimization in aerospace engineering.
In this paper, we take a design-led perspective on the use of computational tools in the aerospace sector. We briefly review the current state-of-the-art in design search and optimization (DSO) as applied to problems from aerospace engineering, focusing on those problems that make heavy use of computational fluid dynamics (CFD). This ranges over issues of representation, optimization problem fo...
متن کاملApproximation Algorithms for Reliable Stochastic Combinatorial Optimization
We consider optimization problems that can be formulated as minimizing the cost of a feasible solution wx over an arbitrary combinatorial feasible set F ⊂ {0, 1}n. For these problems we describe a broad class of corresponding stochastic problems where the cost vector W has independent random components, unknown at the time of solution. A natural and important objective that incorporates risk in...
متن کاملMechanical and Aerospace Engineering
Paper copyrights are retained by the authors, however, The Spectra retains the right to non-exclusive use in print and electronic formats for all papers submitted for publication in The Spectra. PECTR S A 2 Hannah Meredith is a fourth year bio-medical engineering student from Richmond, Virginia. She has been involved with The Spectra since its inception in 2009, serving as a primary editor, Ass...
متن کاملDocToral PrograM in aeroSPace engineering
The aim of the course is the acquisition of the high level competence required to carry out innovative research and/or state of the art advanced applications in industries, public or private research centers, Universities or public and service companies in the area of aerospace engineering, including all the fields associated to it. The level of the course allows the graduates to compete in a E...
متن کاملRobust Integral Sliding-Mode Control of an Aerospace Launch Vehicle
An analysis of on-line autonomous robust tracking controller based on variable structure control is presented for an aerospace launch vehicle. Decentralized sliding-mode controller is designed to achieve the decoupled asymptotic tracking of guidance commands upon plant uncertainties and external disturbances. Development and application of the controller for an aerospace launch vehicle during a...
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: IFAC-PapersOnLine
سال: 2019
ISSN: 2405-8963
DOI: 10.1016/j.ifacol.2019.11.198