Every Quadrotor Needs This Failsafe Software
spectrum.ieee.org
spectrum.ieee.org
I guess what I'm saying is: this software looks really cool but I doubt it will solve my current issues :)
It looks like Real Flight has quadcopters.
still cool (still very much patent pending, too, so also very uncool)
By the way I'm building a community to help RC builders show off their builds. Take a look at some of the vehicles here http://www.rcbinder.com/vehicles . This is my latest build http://www.rcbinder.com/vehicles/aphid-quad
SNORT HAHAHAHA... ok, sorry.
But seriously, even if a patent has been applied for, does that automatically mean everyone else has to stop using it? I don't think that's how it works just based on how easily a process like that could be abused. In reality they should have a few years before it becomes a legit patent right? A lot of things can change in that amount of time.
http://www.uspto.gov/patents/resources/general_info_concerni...
A patent generally does not protect until it has been issued. However:
http://www.irmi.com/expert/articles/2006/warren01.aspx
35 U.S.C. § 154(d) provides "provisional patent rights", namely a "reasonable royalty" after the patent is published (usually 12-18 mos after application) but before it is issued (from 1-30? years). But you do have to have "actual notice" that you are infringing to be infringing, which probably means a notice from the patent applier. (Though if they can prove you watched a YouTube video demonstrating the patent and which said it was patent pending, that'd probably work too.)
So: someone can notify you that you're infringing on a patent in progress, and you have to guess whether or not it will get granted and in what form. Though the answer is unlikely to be "denied", it's quite possible for the claims to mutate tremendously. If you keep going and it gets granted, you've a lawsuit on your hands with liability from date of notice, not date of grant. Fun!
Feel free then, to infringe on any patent that has been described by the applicant but not yet been published by the USPTO. After that, you've got until they catch you (though that's a dangerous game: you're only a friendly jury away from trouble, as the law on "notice" seems not entirely settled.)
What a great system, eh?
Though in US law it seems non-commercial/experimental isn't a complete mitigation as it is elsewhere.
Edit: a brief check on the current US situation shows it's been eroded dramatically and that, like the copyright contract, the patent contract has become a far weaker deal for the public.
Also hope their patent fails. Physics should not be patentable.
if they could fly a quad copter with only one rotor, the engineering behind that is according yo me good enough to allow a patent.
Imagine a copter with reversible motors that can respond quickly-enough (weasel words!) to inputs from the control system. Now, the copter has angular momentum along the direction perpendicular to the rotor disk and a vector between the copter's center of mass and the working motor, and further that the copter is oriented such that the vector is also parallel to the plane of the ground.
As jfoutz said, running the motor ("forward") when the copter is upright and off otherwise gives you net upward thrust (averaged over time). It also applies a torque to the copter, which will mostly be parallel to the extant angular momentum vector. So, a first-order fix is to do what jfoutz said, but also run the motor "backward" (negative thrust) when the copter is upside-down. However, rotor also generates some torque perpendicular to the rotor plane, which will cause the angular momentum vector to rise above the horizon (since the motor reverses when it is upside-down, the angular momentum vector rotates upward rather than revolving around the original direction of the angular momentum vector).
However, if you allow the copter to have some angular momentum (i.e., you don't try to completely eliminate it), the rise might be slow enough to be managed by running the motor at other times. For example, by running the motor when the rotor plane is perpendicular to the ground, you could create a similar drift in the angular momentum vector. But now it slowly drifts around the compass instead of rising above the horizon. If you make the "compass" drift faster than than the "altitude" drift, the torque from the first one will average out to something very small. So by managing the rate of these two drifts with an appropriate feedback loop, you can probably obtain a stable solution where there is a net upward thrust and the angular momentum vector "slowly" (for possibly large values of slow) precesses along the horizon.
Unfortionaly the engines of the hobby quad copters we have today are not reversible without a relay. And even if they where they would not be able to change direction fast enough. One thing that could work is pitchble blades, the problem with that is that it introduces a much bigger risk for failures.
Physics isn't, particular applications of it are. Otherwise, nothing would be patentable. Well, except software.
http://spectrum.ieee.org/automaton/robotics/aerial-robots/ir...
See also:
http://www.itee.uq.edu.au/bme/pounds
... and, if you have IEEE privileges, the paper is here:
http://ieeexplore.ieee.org/xpl/articleDetails.jsp?arnumber=6...
https://fruitychutes.com/uav_rpv_drone_recovery_parachutes/m...
Also, it'd mean either parachute or this failsafe rotation technique. Spinning freakishly like the video shows would only get the quad entangled with a parachute.
However, as unwind mentions, the researchers in the article claim it's possible.
A number of people have built and demonstrated so called 'half prop' helicopters based on the same principle. If you have ever seen an maple seed fall you can understand the principle, search for 'maple copter' on Youtube for some videos of them in action.
In the meantime, the actual linked-to article says "yes":
This new approach allows such a vehicle to remain in flight despite the loss of one, two, or even three propellers. Having lost one (or more) propellers, the vehicle enters a continuous rotation — we then control the direction of this axis of rotation, and the total thrust that the vehicle produces, allowing us to control the vehicle’s acceleration and thus position.