Titlebook: Handbook of Unmanned Aerial Vehicles; Kimon P. Valavanis,George J. Vachtsevanos Reference work 2015 Springer Science+Business Media Dordre

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UAV Design Principles: Introductionepth technical details. It aims at creating the “overall picture” with respect to UAV functionality and, consequently, to indirectly motivate the reader about the challenges that need to be overcome in order to make UAVs fully operational, reliable, and safe.

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Computational and Experimental Design of a Fixed-Wing UAV for the utilization of multi-segmented flight control surfaces on the wings of these UAVs. Adding multiple segments to UAV wings creates smaller control surfaces. By introducing smaller control surfaces, a wing can make refined adjustments to UAV performance while airborne. This unique technique wi

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UAV Handbook: Payload Design of Small UAVsarious small UAV constraints imposed by stringent weight, power, and volume are discussed. Throughout the chapter, the efficacy of these principles is demonstrated with the help of the payloads for a fixed wing UAV developed by the Center for Unmanned Aircraft Systems Research at the U.S. Air Force

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Small UAV Design Development and Sizinge shape of both fueled and electric-powered aircraft. Three examples are given of low-risk UAV configurations. These are shown to be essentially similar from the point of view of optimization and sizing. The sizing methodology for fueled aircraft is described in detail, and a similar one for electri

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Systematic Design Methodology and Construction of Micro Aerial Quadrotor Vehicleshe guideline details the steps to design a stable quadrotor with not more than 50 g takeoff weight while having a flight duration of 8 min. Optimization was done to all mechanical parts of the vehicle with the constraints of its weight and its performance. The guideline first covers the structural a

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Kinematics and Dynamics of Fixed-Wing UAVsics and dynamics of motion, and the transformation of forces and moments acting on the airplane. The detailed discussion of the “kinematics–dynamics–actions” triad in application to a generic fixed-wing UAV is the main objective of this chapter. Therefore, the presentation starts with an introductio

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Dynamic Model for a Miniature Aerobatic Helicopterplified analytical expressions for the component forces and moments. Flight- test experiments were used to estimate several key parameters, such as the equivalent torsional stiffness in the hub. The model was used to design control logic for aerobatic maneuvers performed entirely under computer cont