[NSRCA-discussion] Max volts

Vicente "Vince" Bortone vicenterc at comcast.net
Wed Mar 3 07:41:01 AKST 2010


I believe that those are "open loop" so they are permitted.  

Vicente "Vince" Bortone 

----- Original Message ----- 
From: "Tim Pascoe [Burlington]" <Tim.Pascoe at ec.gc.ca> 
To: "General pattern discussion" <nsrca-discussion at lists.nsrca.org> 
Sent: Wednesday, March 3, 2010 10:35:33 AM GMT -06:00 US/Canada Central 
Subject: Re: [NSRCA-discussion] Max volts 




In reading this, it seems the logic programming available in radios such as the 14MZ, which permit rate changes automatically based on single or multiple stick positions would be illegal. So when I set a condition to drop the Elevator rate by half as soon as full Elevator and full Rudder are initiated, at the entry to a snap, I seem to breaking Number 3 in the Not Permitted list below. 



Correct? 




Tim Pascoe 




From: nsrca-discussion-bounces at lists.nsrca.org [mailto:nsrca-discussion-bounces at lists.nsrca.org] On Behalf Of Earl Haury 
Sent: Wednesday, March 03, 2010 11:02 AM 
To: General pattern discussion 
Subject: Re: [NSRCA-discussion] Max volts 





Somewhat reluctantly I'm going to jump into this discussion and try to dissect it a bit. It appears to me that maybe more is being read into the rules than is actually there. There is one paragraph of three sentences that addresses what type of control is permitted  and what is not. Then there are some examples of what is permitted and what is not. (See below.) "Examples" by definition aren't all inclusive. I think we probably all agree on the "open loop" concept. The ESC discussion seems to fall somewhere in the "auto-pilot exclusion" and  "automatic control sequencing (pre-programming) or automatic control timing device" prohibition seems to be where this discussion lies. 

What's being proposed for ESC functionality, as I understand it, would ensure the same prop speed for a given throttle stick position. Not much difference than a fuel supply control system that ensures the same fuel delivery to the engine at a given throttle position. In neither case is the propulsion system controlling aircraft speed via a feedback loop, the nut on the stick is doing that. Seems OK within the rules to me. 

OTOH, I understand the view that control algorithms are doing magic changing "timing" of electrical pulses to the motor. I would argue this is outside the "automatic control timing device" rule which was intended to prevent automatic "control" inputs directly. Yes - I was around when these rules were discussed and implemented, so I have some insight at to their intent. I also realize that there are things around now that weren't at that time that merit these discussions. It would seem that if everyone feels passionately enough about this an easy fix would to add a sentence (pro or con) in the examples part of the rule that is specific to this topic, therefore keeping the "worms in the can". 

Hmmm as Dave says - I wonder how the control algorithms of a servo fit into this, lots of electronic magic going on there. 

Earl 

"Radio equipment shall be of the open loop type (ie no electronic feedback from the model aircraft 

to the ground). Auto-pilot control utilising inertia, gravity or any type of terrestrial reference is 

prohibited. Automatic control sequencing (pre-programming) or automatic control timing devices 

are prohibited. 

Example: Permitted: 

1. Control rate devices that are manually switched by the pilot. 

2. Any type of button or lever, switch, or dial control that is initiated or activated and terminated 

by the competitor. 

3. Manually operated switches or programmable options to couple and mix control functions. 

SC4_Vol_F3_Aerobatics_09 Effective 1st January 2009 Page 10 

5 

Not permitted: 

1. Snap roll buttons with automatic timing mode. 

2. Pre-programming devices to automatically perform a series of commands. 

3. Auto-pilots or gyros for automatic wing levelling or other stabilisation of the model aircraft. 

4. Propeller pitch change with automatic timing mode. 

5. Any type of voice recognition system. 

6. Conditions, switches, throttle curves, or any other mechanical or electronic device that will 

prevent or limit maximum power or rpm of the propulsion device during the sound/noise test. 

7. Any type of learning function involving manoeuvre to manoeuvre or flight to flight analysis." 




----- Original Message ----- 


From: Dave 


To: 'General pattern discussion' 


Sent: Wednesday, March 03, 2010 9:47 AM 


Subject: Re: [NSRCA-discussion] Max volts 






Matt, 



One more thought/consideration/question – 



Is electronic ignition with variable timing advance illegal?  Essentially the RPM is sensed (through a sensor), and as RPM increases, the timing is advanced.  The ESCs of today do the same function…they advance timing as RPM increases, but do so without sensor.  Should we go back to sensors and mechanical advance devices? 



Regards, 



Dave 












On Mar 2, 2010, at 8:15 AM, rcmaster199 at aol.com wrote: 






I had a brief conversation with Dean Pappas on this subject recently. Dean explained that some folks have been advocates of programming the ESC to do some footwork at various stages of battery use. He explained to me just how easy this is to do physically. It seems a few have mentioned something similar in this thread. 





I am not that concerned about raising the voltage of the battery as I see this as a somewhat clear violation of the FAI code. I am more concerned about what and how the ESC is "programmed" . I would like for some one with the electronic/software pedigree to explain to me how programming adjustable rates of voltage potential and making these adjustments automatically, does not constitute a programming violation within the rules as they exist today. 





When the rules were written, we were clearly dealing with RADIO pre-programmed sequences and the like, no gyros, etc. However I would argue that rate auto adjustments that are definitely possible with the ESC's of today, also qualify as a violation of said rules. Someone should sit down and think this through...I could be convinced otherwise but it needs to be a good argument 





MattK 




  




-----Original Message----- 
From: Anthony Romano < anthonyr105 at hotmail.com > 
To: nsrca-discussion at lists.nsrca.org 
Sent: Tue, Mar 2, 2010 8:29 am 
Subject: Re: [NSRCA-discussion] Max volts 


Keep this line of thinking in mind next time we talk about weight limits! Or any other rules proposal. 
  
Anthony 
  
> From: burtona at atmc.net 
> To: nsrca-discussion at lists.nsrca.org 
> Date: Mon, 1 Mar 2010 22:45:57 -0500 
> Subject: Re: [NSRCA-discussion] Max volts 
> 
> OK, So I have a question. Is knowingly and purposefully violating the intent 
> and letter of the rules to gain a performance advantage called cheating? 
> ....... Just asking! 
> Dave Burton 
> 
> -----Original Message----- 
> From: nsrca-discussion-bounces at lists.nsrca.org 
> [ mailto:nsrca-discussion-bounces at lists.nsrca.org ] On Behalf Of James Oddino 
> Sent: Monday, March 01, 2010 7:16 PM 
> To: General pattern discussion 
> Subject: Re: [NSRCA-discussion] Max volts 
> 
> I have the functional concept that solves the rules problem. Picture a 10S 
> pack positive lead wired to the common of a switch with two poles, a piece 
> of wire connected from one pole to a pole on a second two pole switch with 
> its common connected to the ESC. Between the other two poles we place our 
> 11th cell. When the 10S pack is above 37.5 volts the 11th cell is bypassed 
> and when it is below, like it will be during vertical maneuvers late in 
> flight, the 11th cell is put in series to boost the voltage to up to 41.7 
> volts. At no time is the voltage over the spec. 
> 
> Having said that, I believe the 10S system provides adequate power with the 
> right motor at all times of flight even if the voltage drops to 35 volts. 
> 
> Jim 
> 
> 
> On Mar 1, 2010, at 8:59 AM, Bob Kane wrote: 
> 
> > Going higher and regulating down would be against the rules, the max volts 
> is still limited to 42.56. 
> > 
> > Bob Kane 
> > getterflash at yahoo.com 
> > 
> > 
> > --- On Mon, 3/1/10, krishlan fitzsimmons < homeremodeling2003 at yahoo.com > 
> wrote: 
> > 
> >> From: krishlan fitzsimmons < homeremodeling2003 at yahoo.com > 
> >> Subject: Re: [NSRCA-discussion] Max volts 
> >> To: chad at f3acanada.org , "General pattern discussion" 
> < nsrca-discussion at lists.nsrca.org > 
> >> Date: Monday, March 1, 2010, 9:54 AM 
> >> 
> >> Couldn't we go to a higher voltage and 
> >> regulate it back down? A contstant 42.56v would be nice! 
> >> 
> >> Chris 
> >> 
> >> 
> >> 
> >> 
> >> 
> >> 
> >> 
> >> 
> >> 
> >> From: Chad 
> >> Northeast < chad at f3acanada.org > 
> >> To: 
> >> nsrca-discussion at lists.nsrca.org 
> >> Sent: Sun, 
> >> February 28, 2010 8:48:48 PM 
> >> Subject: Re: 
> >> [NSRCA-discussion] Max volts 
> >> 
> >> You would be at about 50% capacity at 3.85 ish volts/cell 
> >> (resting open circuit), so unless you up the capacity you 
> >> will have a pretty restricted flight time. 
> >> 
> >> Chad 
> >> 
> >> On 10-02-28 9:25 PM, Ron Van Putte wrote: 
> >>> That stirs a wild thought in my brain. Fully 
> >> charged packs don't stay at 4.2 volts per cell very 
> >> long. On the other hand, once the initial charge 
> >> voltage is burned off by a constant load, the voltage loss 
> >> curve "flattens out". What if you put fully 
> >> charged 6S and a 5S packs in series and "burn them 
> >> down" to 3.869 volts per cell (a total of 42.56 
> >> volts for an 11-cell pack) so they were legal for 
> >> use. Would the voltage of this depleted 11S pack be 
> >> higher than a fully charged 10S pack at the end of a typical 
> >> flight? If the end-of-flight voltage might be 
> >> significantly higher for the 11S pack vice a 10S pack, it 
> >> would be worth investigating, even considering the extra 
> >> weight of the additional cell. Come on you electronic 
> >> gurus, show me where I'm wrong. 
> >>> 
> >>> Ron Van Putte 
> >>> 
> >>> On Feb 28, 2010, at 10:00 PM, James Oddino wrote: 
> >>> 
> >>>> What comes after ...? Does it specify a load 
> >> or any other conditions? Is it measured during the 
> >> noise test and have a minimum value? 
> >>>> 
> >>>> Just stirring the pot, Jim O 
> >>>> 
> >>>> 
> >>>> On Feb 28, 2010, at 5:21 PM, John Fuqua wrote: 
> >>>> 
> >>>>> No its not (assuming we are talking RC 
> >> Aerobatics). Try page RCA-2 para 4.1 
> >>>>> which 
> >> states "Electrically-powered model aircraft are 
> >> limited to a maximum 
> >>>>> of 42.56 volts.." 
> >>>>> 
> >>>>> -----Original Message----- 
> >>>>> From: nsrca-discussion-bounces at lists.nsrca.org 
> >>>>> [ mailto:nsrca-discussion-bounces at lists.nsrca.org ] 
> >> On Behalf Of Ron Van Putte 
> >>>>> Sent: Sunday, February 28, 2010 7:07 PM 
> >>>>> To: General pattern discussion 
> >>>>> Subject: Re: [NSRCA-discussion] Max volts 
> >>>>> 
> >>>>> It's in the general rules, not in the R/C 
> >> section. 
> >>>>> 
> >>>>> 
> >>>>> On Feb 28, 2010, at 6:50 PM, Jim Quinn wrote: 
> >>>>> 
> >>>>>> Where can I find the rule 
> >> for max volts? 
> >>>>>> 
> >>>>>> 
> >> _______________________________________________ 
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> >>>>> 
> >>>>> 
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