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Modeling of Fixed wing UAV for Fightgear and Designing its Autopilot in MATLAB Simulink 77 "A" EC

By: Baber Ali; Prof Nadir Munir and sohail Ahmed (Advisors)Publisher: Islamabad NUST 2014Description: v,63pDDC classification: PR 2472

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Item type	Current location	Home library	Collection	Call number	Status	Date due	Barcode	Item holds
Book	College of Aeronautical Engineering (CAE)	College of Aeronautical Engineering (CAE)	NFIC	PR 2472 (Browse shelf)	Available		CAEPR-2472

Total holds: 0

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Previous	PR 247 Study of turbine blade cooling methods and indefifying their effects on turbine performance	PR 2470 CFD Analysis of JF-17 Wing with Control Deflection (Phase-I)	PR 2471 Multi Disciplinary Design Optimization of an Aircraft	PR 2472 Modeling of Fixed wing UAV for Fightgear and Designing its Autopilot in MATLAB Simulink	PR 2473 Constrained Torsional Analysis of Multicell Composite Thin Walled Tapered Beams	PR 2474 Conceptual Desig of a Dual-mode Scramjet Propulsion System for Integration to a Hypersonic Cruise Vehicle in Booster Configuration	PR 2475 Numerical Simulation Based Assessment for Stage-separation Aerothermodynamics of a Pick-a-back Two-stage-to-orbit (TSTO) Space plane configuration	Next

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