Experienced Autonomous Systems Engineer specialising in defence, adept at developing Remote Autonomous Systems.

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Dewi Madden  • Peerlist

Development of a modular MATLAB program to compute the design specifications needed for a light aircraft. Design requirements can be specified and the aircraft performance characteristics will be generated as an output.

Aerospace Design MATLAB Programme

Developing a Boeing 737NG Flight Management Computer tutorial for Aerospace Engineering with Pilot Studies students. Covering a range of areas from route programming to performance data inputs.

Boeing 737NG Flight Management Tutorial

Objective of the project was to utilise GMSH (open source meshing software) to design a Nonweiler Hypersonic Waverider vehicle for analysis in OpenFOAM. This was working in collaboration with Professor V Theofilis of the University of Liver

Design, Development and Predicted Performance of a Nonweiler Caret Waverider using GMSH and Prandtl Meyer Theory

As part of an Aerospace Design module at the University of Liverpool, the aim is to design an ultralight aircraft. Additionally, a cost analysis and performance specification will be generated.

Design of a light Aircraft

The aim of this project was to develop an aircraft that could be sent on a one way mission to a disaster zone then re-engineered to build a human resource (such as a wind turbine or water filter). As the project manager for my group, we dev

Development of an Unmanned Aerial System (UAS) for Humanitarian Relief

Individual Third Year project investigating the dynamics, control and handling qualities of the Boeing 747, one of Boeing's greatest long range aircraft. 

Data taken from: 
Robert K. Heffley and Wayne F. Jewell, Aircraft Handling Qualities

Dynamics, Control and Handling Qualities of the Boeing B747

To analyse and assess the predicted handling qualities of a FastJet to the observed handling qualities using FlightLab software. 

Flight Handling Qualities specifications used: MIL-K-1797A/MIL-F-8785C

Flight Handling Qualities of a FastJet

The objective of this Coursework is to compute flow around a given two-dimensional NACA airfoil, using the Reynolds-averaged Navier-Stokes equations as implemented in the open source software OpenFOAM, and compare the predictions with those

Navier Stokes Computations vs. Potential Flow Theory Predictions

Developed assessment material for Solids and Structures (ENGG110) and Fluid Mechanics (ENGG113) for the University of Liverpool. The content will be used in first year problem classes that will contribute to their overall grade. The project

Structural Engineering and Fluid Mechanics Education Resources (Enhancement Project)

Group 1 will design and develop a UAV for monitoring of breeding pairs of Great Cormorants on Puffin Island in North Wales. The BWBUAV shall collect data that will allow for an estimate of the population of Cormorants on the Island and will