Purpose – This paper aims to propose a spreadsheet method for modeling and simulation of a retraction system mechanism for the retractable self-launching system for a high-performance glider. Design/methodology/approach – More precisely, the method is based on parametric link design using Excel spreadsheets. Findings – This method can be used for kinematic and dynamic analysis, graphical plotting and allows simulation of control kinematics with the ability to make quick and easy parametric changes to a design. It also has the ability to calculate the loads imposed on each component in the control system as a function of input loads and position. Practical implications – This paper shows that it is possible to model complex control systems q...
This thesis sets out to study as many variables of the flight of an F2A Speed category control line ...
This article presents a simulation model in Matlab Simulink used to simulate the gimbal movement. Th...
This report consists of two parts. In the first part we will discuss a so-called bottom-up approach ...
Purpose This paper aims to propose a spreadsheet method for modeling and simulation of a retraction...
The simulation presented in this thesis illustrates some of the basic mechanisms governing the winch...
automatic adjustment user’s edit Figure 1: (Left) Our model airplane design tool analyzes the aerody...
In this paper we develop the study of the oscillatory movement of a mass-spring system to illustrate...
Thesis (M.Ing. (Mechanical Engineering)--North-West University, Potchefstroom Campus, 2010.In this p...
i In this project a preliminary design of a self-launching system for the JS1 sailplane was attempte...
Development of modern aircraft has become more and more expensive and time consuming. In order to mi...
The paper deals with the high-fidelity modeling and simulation of a powered parafoil-payload system ...
The design and simulation of an adaptive longitudinal control system for a Mach 8 hypersonic glider ...
Attribution License, which permits unrestricted use, distribution, and reproduction in any medium, p...
A spreadsheet-aided engineering design tool has been developed to assist in the parachute design pro...
abstract: This thesis will cover the basics of 2-dimensional motion of a parafoil system to determin...
This thesis sets out to study as many variables of the flight of an F2A Speed category control line ...
This article presents a simulation model in Matlab Simulink used to simulate the gimbal movement. Th...
This report consists of two parts. In the first part we will discuss a so-called bottom-up approach ...
Purpose This paper aims to propose a spreadsheet method for modeling and simulation of a retraction...
The simulation presented in this thesis illustrates some of the basic mechanisms governing the winch...
automatic adjustment user’s edit Figure 1: (Left) Our model airplane design tool analyzes the aerody...
In this paper we develop the study of the oscillatory movement of a mass-spring system to illustrate...
Thesis (M.Ing. (Mechanical Engineering)--North-West University, Potchefstroom Campus, 2010.In this p...
i In this project a preliminary design of a self-launching system for the JS1 sailplane was attempte...
Development of modern aircraft has become more and more expensive and time consuming. In order to mi...
The paper deals with the high-fidelity modeling and simulation of a powered parafoil-payload system ...
The design and simulation of an adaptive longitudinal control system for a Mach 8 hypersonic glider ...
Attribution License, which permits unrestricted use, distribution, and reproduction in any medium, p...
A spreadsheet-aided engineering design tool has been developed to assist in the parachute design pro...
abstract: This thesis will cover the basics of 2-dimensional motion of a parafoil system to determin...
This thesis sets out to study as many variables of the flight of an F2A Speed category control line ...
This article presents a simulation model in Matlab Simulink used to simulate the gimbal movement. Th...
This report consists of two parts. In the first part we will discuss a so-called bottom-up approach ...