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
this is the link of our imu http://www.flickr.com/photos/44555417@N04/page2/