Solving Flow Balancing Problem for Hybrid-Electric Aircraft Cooling Systems

the algorithm for solving the inverse numerical range problem

برد عددی ماتریس مربعی a را با w(a) نشان داده و به این صورت تعریف می کنیم w(a)={x8ax:x ?s1} ، که در آن s1 گوی واحد است. در سال 2009، راسل کاردن مساله برد عددی معکوس را به این صورت مطرح کرده است : برای نقطه z?w(a)، بردار x?s1 را به گونه ای می یابیم که z=x*ax، در این پایان نامه ، الگوریتمی برای حل مساله برد عددی معکوس ارانه می دهیم.

Hybrid Genetic-cuckoo Search Algorithm for Solving Runway Dependent Aircraft Landing Problem

As the demand for air transportation continues to grow, some flights cannot land at their preferred landing times because the airport is near its runway capacity. Therefore, devising a method for tackling the Aircraft Landing Problem (ALP) in order to optimize the usage of existing runways at airports is the focus of this study. This study, a hybrid Genetic-Cuckoo Search (GCS) algorithm for opt...

Stability Analysis and Control Design for Hybrid Ac-dc More- Electric Aircraft Power Systems

VizCraft: a problem-solving environment for aircraft configuration design

understanding of their data that was not previously possible. However, lack of integration among the various software modules often separates the visualization process from the computation that generates the data. VizCraft is a problem-solving environment that aids designers during the configuration design of a high-speed civil transport (HSCT). VizCraft provides a graphical user interface to a...

Flow Balancing Nonlinear Systems

This paper introduces a novel approach towards balancing of nonlinear systems. It differs from other approaches in two key ideas: The first is the observation that linear timeinvariant systems have a single equilibrium point (the origin), and that the balanced realization for the class of a linear timeinvariant systems essentially relates to this equilibrium. This sparked the idea to consider b...