MIT ACL - Variable Pitch Quadrotor
AerospaceControlsLab1 HN recommenders · 2013–2016
133K views · demo · evergreen · Uploaded 2011-07-08
A short MIT Aerospace Controls Lab demo from 2011 of a variable pitch quadrotor flying.
Referenced in drone threads as a demonstration that variable pitch quadcopters fly well with little drift.
15:01What Happened to Horses Is Happening to Us
CGP Grey
25:33Children Of The Magenta Line
Mossie Fly
11:38The Economics of Airline Class
Wendover Productions
3:56:24David Fravor: UFOs, Aliens, Fighter Jets, and Aerospace Engineering | Lex Fridman Podcast #122
Lex Fridman
8:28The Fastest Way to Board a Plane Feels Like the Slowest
CGP Grey
11:46Zipline - How Rwanda Built A Drone Delivery Service
Real Engineering
1:49:56Pulling Power from the Sky: The Story of Makani [Feature Film]
X, The Moonshot Factory
1:54:26Joe Rogan Experience #1361 - Cmdr. David Fravor & Jeremy Corbell
PowerfulJRE
3 comments from Hacker News
Are there other types of drones other than traditional quadcopters, for example variable-pitch quadcopters [1], that can get more airspeed and thus cover more distance in 15 min? What about using airplane-style drones (like traditional RC planes) + a parachute to land the package? And this way you could use nitro gas fuel to get better energy density (since you can use one big gas engine instead of having to use four tiny motors) [1] [VIDEO]
Manned multicopters have already happened. [1] MIT has also demonstrated a variable pitch quadcopter. [2] If they can use plasma laminar detachment and reattachment to somehow simulate a variable pitch propeller, while still getting some weight savings over a design with multiple swashplates, then yes I think it should help the quadcopter design scale up to larger propellers. That's a big if though, since to simulate a negative angle of attack I'm guessing your propeller design would have to be pretty inefficient with all plasma turned off. I'm not entirely sure why you want this though, since the single large rotor is more efficient. There was a novel design a few years ago with one large rotor for lift and three smaller ones to counter torque and provide control. [3] [1] [LINK] [2] [VIDEO] [3] [LINK]
The example you posted has far more things in common with a multirotor than with a helicopter. What amazes me at those little things is how little side-to-side drift they have, considering that's all depending on the CG being well centered. A nice variable pitch quad: [VIDEO]