Ducted Fan 'AirMule' UAS Completes First Phase of Flight Testing | Aero-News Network
Aero-News Network
RSS icon RSS feed
podcast icon MP3 podcast
Subscribe Aero-News e-mail Newsletter Subscribe

Airborne Unlimited -- Most Recent Daily Episodes

Episode Date

Airborne-Monday

Airborne-Tuesday

Airborne-Wednesday Airborne-Thursday

Airborne-Friday

Airborne On YouTube

Airborne-Unlimited-04.29.24

Airborne-Unlimited-04.23.24

Airborne-Unlimited-04.24.24 Airborne-FltTraining-04.25.24

Airborne-Unlimited-04.26.24

Sun, Jan 17, 2010

Ducted Fan 'AirMule' UAS Completes First Phase of Flight Testing

Urban Aeronautics’ Rotorless VTOL Aircraft Demonstrates Hover Capability

The AirMule, a single-engine, VTOL Cargo and MedEvac UAS developed by Israel-based Urban Aeronautics, has successfully completed the first phase of its flight testing. This phase has consisted of tethered autonomous hovers with the vehicle’s Fly-By-Wire control system providing the necessary auto-stabilization in all three rotational axes of the vehicle ... pitch, roll and yaw.

Control of the vehicle is accomplished through a company developed, four channel, redundant flight control system that relies almost entirely on inertial measurements augmented by GPS for translational position and velocity readings. Height above ground is measured by two laser altimeters. 460 channels of telemetry provide real-time data to the ground based operators, enabling them to monitor the correct operation of the Turbomeca Arriel1 730 horsepower turbo-shaft engine as well as sub-systems.  These include the three company developed gearboxes, the two main lift rotors with their hydraulic pitch change mechanism and three uplink and downlink communication channels.

Results from the tests have confirmed the company’s predictions regarding power required for hover. The present hover height of approximately 2 feet is just outside of ground effect for this particular configuration. The aircraft uses a system of vanes for yaw and roll control, and in the test demonstrated the vehicle’s ability to perform hover with very high precision in gusty wind conditions (currently estimated and confirmed by the recent hover tests at 50 knots for the fully developed product).

Based on the success of these initial hover tests the vehicle is now being readied for the next phase which will include vehicle position stabilization in X,Y and height above ground.  During this upcoming phase the safety wires that are now connected to the tarmac will be removed.

FMI: www.urbanaero.com 

Advertisement

More News

ANN's Daily Aero-Term (04.28.24): Airport Marking Aids

Airport Marking Aids Markings used on runway and taxiway surfaces to identify a specific runway, a runway threshold, a centerline, a hold line, etc. A runway should be marked in ac>[...]

Aero-News: Quote of the Day (04.28.24)

"It is extremely difficult, if not impossible, for manned aircraft to see a drone while conducting crop-enhancing and other aerial applications at low altitudes and high speeds. We>[...]

ANN's Daily Aero-Linx (04.28.24)

Aero Linx: The Skyhawk Association The Skyhawk Association is a non-profit organization founded by former Skyhawk Pilots which is open to anyone with an affinity for the A-4 Skyhaw>[...]

Aero-News: Quote of the Day (04.29.24)

“The T-54A benefits from an active Beechcraft King Air assembly line in Wichita, Kansas, where all required METS avionics and interior modifications are installed on the line>[...]

ANN's Daily Aero-Linx (04.29.24)

Aero Linx: Aerostar Owners Association The Association offers the Aerostar Owner a unique opportunity to tap an invaluable source of information concerning the care and feeding of >[...]

blog comments powered by Disqus



Advertisement

Advertisement

Podcasts

Advertisement

© 2007 - 2024 Web Development & Design by Pauli Systems, LC