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Determination and evaluation of UAV safety objectives
R Clothier, R Walker - … of the 21st international conference on …, 2006 - eprints.qut.edu.au
The integration and acceptance of routine Unmanned Aerial Vehicle (UAV) operations
within the civilian airspace system hinges on the ability of UAV developers, operators and …
within the civilian airspace system hinges on the ability of UAV developers, operators and …
Design and flight testing of inflatable wings with wing war**
The paper presents work on testing of inflatable wings for unmanned aerial vehicles (UAVs).
Inflatable wing history and recent research is discussed. Design and construction of …
Inflatable wing history and recent research is discussed. Design and construction of …
BIG BLUE: high-altitude UAV demonstrator of Mars airplane technology
AD Simpson, OA Rawashdeh, SW Smith… - 2005 IEEE …, 2005 - ieeexplore.ieee.org
BIG BLUE (baseline inflatable-wing glider, balloon-launched unmanned experiment) is a
flight experiment envisioned, designed, built, and flown primarily by undergraduate students …
flight experiment envisioned, designed, built, and flown primarily by undergraduate students …
Development of a finite element model of war** inflatable wings
This paper presents development of a structural model of war** inflatable wings. In order
to quickly and effectively analyze the effects of aerodynamic loading and to consider design …
to quickly and effectively analyze the effects of aerodynamic loading and to consider design …
Design and evaluation of inflatable wings for UAVs
AD Simpson - 2008 - uknowledge.uky.edu
Performance of inflatable wings was investigated through laboratory, wind tunnel and flight-
testing. Three airfoils were investigated, an inflatable-rigidazable wing, an inflatable …
testing. Three airfoils were investigated, an inflatable-rigidazable wing, an inflatable …
Multidisciplinary design experience of a high altitude inflatable wing UAV for aerospace workforce development
NASA is addressing the anticipated shortage of aerospace engineers in part through
workforce development projects of the National Space Grant College and Fellowship …
workforce development projects of the National Space Grant College and Fellowship …
Big blue II: Mars aircraft prototype with inflatable-rigidizable wings
The present paper presents work on develo** and flight testing a Mars prototype aircraft
using inflatable-rigidizable wings under the NASA Workforce Development program …
using inflatable-rigidizable wings under the NASA Workforce Development program …
Design and realization of an unmanned aerial rotorcraft vehicle using pressurized inflatable structure
N Sadasivan - International Journal of Aviation, Aeronautics, and …, 2019 - commons.erau.edu
Unmanned aerial rotorcraft vehicles have many military, commercial and civil applications.
There is a necessity to advance the performance on several ranges of rotorcraft for using …
There is a necessity to advance the performance on several ranges of rotorcraft for using …
Historical perspective on inflatable wing structures
W Pulliam, R Norris - 50th AIAA/ASME/ASCE/AHS/ASC Structures …, 2009 - arc.aiaa.org
Inflatable aerodynamic structures have begun to find uses in specialized aircraft that require
storage in small volumes or morphing to improve cruise performance. Although inflatables …
storage in small volumes or morphing to improve cruise performance. Although inflatables …
Conceptual Design and Sizing of a Solar Powered Tilt-Rotor Hybrid UAV for exploration over Mars
P Gupta, AJ Poojary, RS Pant - AIAA AVIATION 2023 Forum, 2023 - arc.aiaa.org
View Video Presentation: https://doi. org/10.2514/6.2023-4070. vid This paper presents a
comprehensive analysis of conceptual sizing for a solar-powered Unmanned Aerial Vehicle …
comprehensive analysis of conceptual sizing for a solar-powered Unmanned Aerial Vehicle …