Hello everyone,
in this video you can see the first pre-flight testing on the new HG3.2 the airplane has the following features:
Created by Joseph D'Angelo
Hardware and firmware development: Roberto Navoni
Electronic Edge: Ardubotix 1.0A (Multipilot)
Wheelbase: 1.65 m
Maximum dimensions: 2.60 x 2.60 m
V2 Version: hybrid
Electric Motor: Hacker A60
Petrol Engine: Zenoah
Blades: SAB Composite
Frame: DIY
Here we can found the video : http://www.virtualrobotix.com/profiles/blogs/hg32-preflight-check
Here you can found the full story : http://www.virtualrobotix.com/profiles/blogs/hg3-the-era-of-quad-variable
Blog of Giuseppe Pipposoft for the friends ;) : http://www.virtualrobotix.com/profile/GiuseppeDAngelo?xg_source=activity
Comments
Infact you though like me and implimented first ;-))
Quadrocopter has its own UAV application for short range surveillance.
This will open new era in the Quadrocopter de sign race..
As I understand, in this setting, it is the rotor pitch which is adjusted with a high frequency instead of the rotation speed and therefore, the rotation speed is constant at each given time for all the rotors. if this is the case, I am wondering how this would affect the stability of the quad in general, and its maneuverability in terms of responsiveness in specific.
Thanks
What is the total flying weight?
What is the function of the Hacker A60 motor?
this is the link of our imu http://www.flickr.com/photos/44555417@N04/page2/