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 …

Design and flight testing of inflatable wings with wing war**

JD Jacob, A Simpson, S Smith - 2005 - sae.org
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 …

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 …

Development of a finite element model of war** inflatable wings

J Rowe, S Smith, A Simpson, J Jacob… - 47th AIAA/ASME/ASCE …, 2006 - arc.aiaa.org
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 …

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 …

Multidisciplinary design experience of a high altitude inflatable wing UAV for aerospace workforce development

J Jacob, J Lumpp, S Smith, W Smith - 44th AIAA Aerospace Sciences …, 2006 - arc.aiaa.org
NASA is addressing the anticipated shortage of aerospace engineers in part through
workforce development projects of the National Space Grant College and Fellowship …

Big blue II: Mars aircraft prototype with inflatable-rigidizable wings

A Simpson, J Jacob, S Smith, O Rawashdeh… - 43rd AIAA Aerospace …, 2005 - arc.aiaa.org
The present paper presents work on develo** and flight testing a Mars prototype aircraft
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 …

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 …

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 …