2nd AIAA "Unmanned Unlimited" Conf. And Workshop &Amp; Exhibit 2003
DOI: 10.2514/6.2003-6567
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A Powered Lift Aerodynamic Analysis for the Design of Ducted Fan UAVs

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Cited by 52 publications
(29 citation statements)
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“…The force generated by a ducted fan is modeled based on models in references [9], [10] and [11]. The fundamental model of a ducted fan is introduced first, then it is extended to the VTAV case.…”
Section: Dynamical Model a Rigid Body Modelmentioning
confidence: 99%
“…The force generated by a ducted fan is modeled based on models in references [9], [10] and [11]. The fundamental model of a ducted fan is introduced first, then it is extended to the VTAV case.…”
Section: Dynamical Model a Rigid Body Modelmentioning
confidence: 99%
“…The superposition of all elements of the model, taking into account any appropriate interaction effects, then yields the summation of all forces and moments acting on the total vehicle airframe. This general approach has been applied to a wide range of problems in modeling and simulation, for example, propellerdominated UAV flight dynamics, 5,6,15 ducted fan configurations, 16 autonomous underwater vehicles, 17 wingonly tumbling analysis, 18 high angle of attack longitudinal aircraft trim analysis, 19 and post-stall flight dynamics and upset modeling [20][21][22][23][24] to name a few.…”
Section: Introductionmentioning
confidence: 99%
“…Helicopters, however, are uneasy to operate in awkward environments due to the exposed rotor blades. Very little has been done on the development of secure platforms (Hamel et al 2002, Fleming et al 2003, Guerrero et al 2003. Such platforms have considerable potential for surveillance and inspection roles in dangerous or constrained environments.…”
Section: Introductionmentioning
confidence: 99%