FOREWORD
Journal Title: INCAS BULLETIN - Year 2009, Vol 1, Issue 2
Abstract
Authors and Affiliations
Catalin NAE
Keywords
Related Articles
- EP ID EP85507
- DOI 10.13111/2066-8201.2009.1.2.1
- Views 133
- Downloads 0
Mathematical modeling of a V-stack piezoelectric aileron actuation
The article presents a mathematical modeling of aileron actuation that uses piezo V-shaped stacks. The aim of the actuation is the increasing of flutter speed in the context of a control law, in order to widen the flight...
Composite material designs for lightweight space packaging structures
This paper presents a study on advanced material designs suitable for lightweight space packaging structures. During this study, several material designs were proposed, evaluated and in the end three packaging structures...
MDO approach for a two-stage microlauncher
The paper focuses on the multidisciplinary optimisation and preliminary design of a two-stage microlauncher capable of inserting a small 50 kg payload into Low Earth Orbit. The microlauncher is obtained using a MDO appro...
Test Rig Adaptation for WT Measurements for OR&TP Configurations
The need to test large models at maximum speed regimes close to 100 m/s, for which the aerodynamic forces and moments occurring on the model far exceed the measuring capability of the existing TEM external balance, made...
Longitudinal automatic control system for a light weight aircraft
This paper presents the design of an automatic control system for longitudinal axis of a light weight aircraft. To achieve this goal it is important to start from the mathematical model in longitudinal plane and then to...