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MULTI-OBJECTIVE OPTIMIZATION OF A STEALTH UNMANNED COMBAT AERIAL VEHICLE

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dc.contributor.author Ammar Akram- Muhammad Fahad Zahid- Muhammad Ahsan Aziz, Supervised By Dr Emad ud Din
dc.date.accessioned 2020-10-23T13:31:27Z
dc.date.available 2020-10-23T13:31:27Z
dc.date.issued 2019
dc.identifier.uri http://10.250.8.41:8080/xmlui/handle/123456789/3951
dc.description.abstract For Unmanned Combat Aerial Vehicles (UCAVs) operating during wartime, the mission objective is dependent on the survivability of the UCAV, which depends on two things: 1. Its ability to evade detection by enemy radars and scanners (Stealth) 2. Its ability to evade enemy fire when detected and fired upon. (Maneuverability). This project entails the optimization of an Unmanned Combat Aerial Vehicle with maximized survivability to be used in conceptual phase of Aircraft Design. This shall be accomplished by means of a Multi-Objective Optimization, employing the Genetic Algorithm, with the objective functions being the Radar Cross Section (RCS) – which is to be minimized, and the Lift-to-Drag Ratio which signifies the Aerodynamic performance – which is to be maximized. Genetic Algorithm for Multi-Objective Optimization from MATLAB Optimization Toolbox is used. To minimize computational expense in the conceptual design phase, low fidelity methods for Lift to Drag Ratio and RCS calculations are used; Vortex Lattice Method (VLM) and Physical Optics (PO), respectively. en_US
dc.language.iso en_US en_US
dc.publisher SMME-NUST en_US
dc.relation.ispartofseries SMME-FYP-164;
dc.title MULTI-OBJECTIVE OPTIMIZATION OF A STEALTH UNMANNED COMBAT AERIAL VEHICLE en_US
dc.type Thesis en_US


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