AeroElectric-List Digest Archive

Mon 04/09/12


Total Messages Posted: 24



Today's Message Index:
----------------------
 
     1. 02:13 AM - Re: Re: ELT Antenna Mount (BobsV35B@aol.com)
     2. 05:40 AM - Re: ELT Antenna Mount (Jared Yates)
     3. 05:50 AM - Re: Conduit in wings. (John Morgensen)
     4. 06:12 AM - Re: Conduit in wings. (Ken)
     5. 06:29 AM - Re: Re: ELT Antenna Mount (Ralph Finch)
     6. 06:43 AM - Re: Re: ELT Antenna Mount ()
     7. 07:07 AM - Re: Re: ELT Antenna Mount (Kelly McMullen)
     8. 07:09 AM - Re: Re: ELT Antenna Mount (BobsV35B@aol.com)
     9. 09:28 AM - Re: Next generation wig-wag controller for LED lamps (gregmchugh)
    10. 09:58 AM - Re: Re: Next generation wig-wag controller for LED lamps (Daniel Hooper)
    11. 10:50 AM - Re: Next generation wig-wag controller for LED lamps (gregmchugh)
    12. 10:50 AM - Who got lost without an ELT? (Paul Millner)
    13. 11:25 AM - Open source product development for OBAM aircraft (Robert L. Nuckolls, III)
    14. 11:38 AM - Re: Re: ELT Antenna Mount (Robert L. Nuckolls, III)
    15. 12:20 PM - Re: Open source product development for OBAM aircraft (Robert L. Nuckolls, III)
    16. 12:42 PM - Re: Open source product development for OBAM aircraft (Daniel Hooper)
    17. 02:12 PM - Re: Open source product development for OBAM aircraft (Robert L. Nuckolls, III)
    18. 02:15 PM - Re: Open source product development for OBAM aircraft (Jeff Luckey)
    19. 03:40 PM - Re: Open source product development for OBAM aircraft (gregmchugh)
    20. 04:47 PM - Re: Open source product development for OBAM aircraft (gregmchugh)
    21. 07:41 PM - Re: Re: Open source product development for OBAM aircraft (Robert L. Nuckolls, III)
    22. 07:50 PM - Re: Re: Open source product development for OBAM aircraft (Robert L. Nuckolls, III)
    23. 08:01 PM - Point me in the right direction (Bill Bradburry)
    24. 09:17 PM - Re: Point me in the right direction (Bruce)
 
 
 


Message 1


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    Time: 02:13:54 AM PST US
    From: BobsV35B@aol.com
    Subject: Re: ELT Antenna Mount
    Good Morning RalphMariaFinch, I use the name above because there is no other salutation or signature on your note. My recollection is that Matt does request that all communications to his list include such information. In any case. I would be happy if the government does not come and look for me. I happily drive my car all over the USA and never ask any governmental agency to follow my track. When I want my travels followed, I use many methods based on where I am traveling, the mode of travel, and the relative danger that might be associated with that travel. The original ELT was and is a basic disaster. Typical of all government programs, it costs more and provides less help than most other methods that are available. The new units are better, but still not as positive as other methods that we can use IF we desire. Personally, I do carry a PLB. I also carry a portable GPS and a portable VHF radio. I also use and encourage my family to use a SPOT. Sure, I may use governmental services if they are available, but I will have chosen the method and evaluated the risk versus cost. Individual choice is the way it should be done. I do not want you or anyone else to pay for a search to find me or my remains. Happy Skies, Old Bob AKA Bob Siegfried Downers Grove, IL Stearman N3977A Bonanza N20318 Do Not Archive In a message dated 4/9/2012 12:22:34 A.M. Central Daylight Time, ralphmariafinch@gmail.com writes: I wouldn't mind if it were optional, but then for those who don't carry one, I don't want to pay taxes to go look for you. The ELT requirement started when a Congresscritter disappeared in his light plane in Alaska and the military spent a lot of time and money looking for him. Never did find him. You can say they're worthless all you want (ELTs, I mean) but since the government spends money to look for you they have the right to force you to make their job easier. On Sun, Apr 8, 2012 at 9:57 AM, <_Speedy11@aol.com_ (mailto:Speedy11@aol.com) > wrote: Old Bob is right on target. ELTs are a government-required waste of money. The decision to carry one should be at the choice of the owner/operator. I don't care if mine works or not. I don't plan to depend on it. As Bob said, "Too many rules driven by pure bureaucracy" Check Six, Old Stan


    Message 2


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    Time: 05:40:24 AM PST US
    Subject: Re: ELT Antenna Mount
    From: Jared Yates <email@jaredyates.com>
    As a side note to the airliner discussion, each airliner that I have operate d (thus far) has had an ELT. As you say, it has been operated under IFR, bu t it has also been followed by a staff of trained and certificated dispatche rs in a well-equipped operations center, complete within fancy computers and back up generators. It's been flown according to pre-planned route, with t wo current, medically certified, qualified crewmembers at the controls. And of course, a staff of operators at the arrival point who have a written pla n for what to do if the airplane doesn't show up on time. We've also carried a CVR and FDR, both of which also have their own locating beacons. Finally , we've carried enough fuel to make a huge smoking hole event crash. Safety i s often in the eye of the beholder, but I think it's an exaggeration to thin k that you have the same level of safety as an airliner when it comes to sea rch and rescue. It's easy for you to say that you don't want any help with S AR, but until the FAA makes that a box that you can check on the flight plan form, I don't see how you're going to opt out from practical standpoint. It 's sort of like believing that you can opt out of the healthcare system- per haps possible but highly unlikely in practice. > I can do at least as good a job of providing guidance for recovery of my a ircraft as do the air carriers. I might elect to fly IFR at all times or I m ay just decide that I do not want any help if I should fail to get where I a m going. > > > > > In a message dated 4/7/2012 1:01:40 P.M. Central Daylight Time, dee.whitti ngton@gmail.com writes: > Bob, > > As I understand it, the reason commercial airliners don't have ELTs is the y are always in contact with ATC and on IFR flight plans. If they crash, the re is no question of locating them unlike a GA airplane which can choose to f ly VFR with no flight plan and not in touch with ATC. > > Dee > > On Sat, Apr 7, 2012 at 1:45 PM, <BobsV35B@aol.com> wrote: > Good Afternoon Tim, > > Maybe the builder feels the same about an ELT as I do. > > Possibly he/she is just trying to be legal but does not care a whit whethe r or not it works! > > My feeling is that the use of an ELT should be a decision for the owner/op erator, NOT a requirement of the law. > > Airliners are not required to carry one. Why should we? > > Too many rules driven by pure bureaucracy. > > Do Not Archive. > > Happy Skies, > > Old Bob > AKA > Bob Siegfried > Brookeridge Air Park > N3977A > > In a message dated 4/7/2012 12:31:03 P.M. Central Daylight Time, tim2542@s bcglobal.net writes: > Well certainly the omni-directional characteristics of the 1/4 wave antenn a are ruined, the vswr, is probably affected, it's horizontally polarized an d nicely shielded......It might still work but you'll never know until you n eed it. If you want to hide ALL the antennas inside structure you probably n eed a glass plane.... ;-) > Tim > Cozy Mk IV > > Sent from my iPad > > On Apr 7, 2012, at 10:32 AM, "Jeff Luckey" <JLuckey@pacbell.net> wrote: > >> Please see attached picture: >> >> >> >> Please understand that my intention is not to be critical, but to learn >> >> >> >> Is this an effective way to mount an ELT antenna? >> >> >> >> I understand why this builder chose to mount it this way. But I have con cerns that there is a great deal of signal-blocking structure very close to t he antenna. >> >> >> >> What do you RF gurus think? >> >> >> >> -RF neophyte >> >> >> >> >> >> > > > ========================== ========= ========================== ========= ========================== ========= ========================== ========= >


    Message 3


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    Time: 05:50:42 AM PST US
    From: John Morgensen <john@morgensen.com>
    Subject: Re: Conduit in wings.
    I used 1/2 inch CPVC pipe and plastic pipe hangers. CPVC is lighter than regular PVC and it used for the hot water lines in motor homes. john On 4/8/2012 6:03 PM, rayj wrote: > > Greetings, > > I'm planning on completing my aircraft with a minimum electrical > system and providing a way to install wingtip lights later. Any > experiences anyone has with using different types of conduit in wings > would be appreciated. > > Thanks in advance, > Raymond Julian > Kettle River, MN > > "And you know that I could have me a million more friends, > and all I'd have to lose is my point of view." - John Prine > >


    Message 4


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    Time: 06:12:03 AM PST US
    From: Ken <klehman@albedo.net>
    Subject: Re: Conduit in wings.
    I've been told by a plastic manufacturer that cpvc is about the worst plastic out there for toxic smoke if it ever does burn. The translucent poly pipe used for things like ice maker water supply lines might be a better choice and more flexible if that matters. Several sizes available. I do favor non conductive conduit rather than metal. It helps to leave a string in the conduit if you plan to pull extra wires through later. The previously mentioned plastic snap in grommets are handy for running conduit through metal ribs. Ken On 09/04/2012 8:48 AM, John Morgensen wrote: > <john@morgensen.com> > > I used 1/2 inch CPVC pipe and plastic pipe hangers. CPVC is lighter than > regular PVC and it used for the hot water lines in motor homes. > > john > > On 4/8/2012 6:03 PM, rayj wrote: >> >> Greetings, >> >> I'm planning on completing my aircraft with a minimum electrical >> system and providing a way to install wingtip lights later. Any >> experiences anyone has with using different types of conduit in wings >> would be appreciated. >> >> Thanks in advance, >> Raymond Julian >> Kettle River, MN >>


    Message 5


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    Time: 06:29:13 AM PST US
    From: Ralph Finch <ralphmariafinch@gmail.com>
    Subject: Re: ELT Antenna Mount
    > > Personally, I do carry a PLB. > > And if you activate that, who will come looking for you? Not your friends or family, but the government, on the taxpayer's dime. So you confirm that you are not as independent as your mythology tells you.


    Message 6


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    Time: 06:43:26 AM PST US
    From: <rd2@dejazzd.com>
    Subject: Re: ELT Antenna Mount
    Not exactly, Robert :) - our numbers are greater than 3 or 4 - there are many more of us who are not relinquishing freedoms for imposed "safety", "well-being", "welfare" etc. But that's beyond the scope of this list. Rumen do not archive ---- Robert Borger <rlborger@mac.com> wrote: > Old Bob & Stan, Guess it makes 3 of us. Blue skies & tailwinds, Bob Borger Europa XS Tri, Rotax 914 w/ Intercooler & Airmaster C/S Prop Little Toot Sport Biplane, Lycoming AEIO-320 EXP 3705 Lynchburg Dr. Corinth, TX 76208-5331 H: 940-497-2123 C: 817-992-1117 On Apr 08, 2012, at 12:18 PM, BobsV35B@aol.com wrote: Hi Stan, Nice to know I am not alone! Happy Skies, Old Bob Do Not Archive In a message dated 4/8/2012 12:00:16 P.M. Central Daylight Time, Speedy11@aol.com writes: Old Bob isright on target. ELTs are a government-required waste of money. The decision to carry one should be at the choice of the owner/operator. I don't care if mine works or not. I don't plan to depend on it. As Bob said, "Too many rules driven by pure bureaucracy" ========================


    Message 7


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    Time: 07:07:39 AM PST US
    From: Kelly McMullen <kellym@aviating.com>
    Subject: Re: ELT Antenna Mount
    Just for accuracy, It wasn't just one congresscritter, it was the House Majority Leader, along with the only House Member for Alaska, along with 2 others in a charter Cessna 310 with a professional, experienced pilot....not just a little light plane out for a joy ride. Perhaps that is why in recent years the Sec. Service has insisted on military aircraft carrying the Majority Leader. BTW Canada had been requiring ELTs for a year or two when this happened. On 4/8/2012 10:19 PM, Ralph Finch wrote: > > The ELT requirement started when a Congresscritter disappeared in his > light plane in Alaska and the military spent a lot of time and money > looking for him. Never did find him. You can say they're worthless all > you want (ELTs, I mean) but since the government spends money to look > for you they have the right to force you to make their job easier.**** ----- No virus found in this message. Checked by AVG - www.avg.com


    Message 8


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    Time: 07:09:22 AM PST US
    From: BobsV35B@aol.com
    Subject: Re: ELT Antenna Mount
    Good Morning ralphmariafinch, Obviously I disagree with every point you mention, but this discussion has no place on this list. It started when I suggested that the builder placing his antenna in that rather unconventional position was like me and did not feel that good performance from the ELT was important. And ---- I still follow Matt's request as to identifying ourselves and as to adding Do Not Archive, to messages of little importance such as this. Happy Skies, Old Bob AKA Bob Siegfried Downers Grove, Illinois Piper Pacer PA-20 In a message dated 4/9/2012 8:29:56 A.M. Central Daylight Time, ralphmariafinch@gmail.com writes: Personally, I do carry a PLB. And if you activate that, who will come looking for you? Not your friends or family, but the government, on the taxpayer's dime. So you confirm that you are not as independent as your mythology tells you.


    Message 9


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    Time: 09:28:00 AM PST US
    Subject: Re: Next generation wig-wag controller for LED lamps
    From: "gregmchugh" <gregmchugh@aol.com>
    Bob, I probably should have changed the Subject line on this but I decided to leave it alone to continue the thread we had started. It is getting away from the LED wig-wag topic... I have thought about this a little and I think it would be worthwhile to consider the option of a general purpose programmable module and use the LED wig-wag as a simple example application. I see three useful characteristics for this module: 1. Functionality set in software 2. Some capability to configure the I/O circuits for each application 3. A standard module package and connector such as the one you showed using an enclosed case with d-sub connector To be useful for a wide audience there needs to be simple learning curve for developing the software functionality and I/O configuration. I agree that the use of a PIC micro would be the way to go based on their ready availability, good price per performance, and availability of development tools. In order to make it attractive for general use I would propose the following: Software Development - The learning curve for using the standard PIC software development tools is pretty steep for a novice and I would expect many would shy away from that learning curve. There are some third party development tools designed to ease the learning curve but at a price of $150 and up they are not targeted at the novice hobbyist. An attractive option is the line of PICAXE micros targeted at the education market and easily applied to the types of applications being considered here (I don't think we are looking at applications that require high performance embedded processing). You can get started with PICAXE development for $25 to $50 depending on which processor and which downloading cable you use. The PICAXE development environment is free and easy to use for the novice with the capability to simulate the micro operation without connection to a micro. The use of a version of BASIC designed for embedded applications makes it easy to program but there is an execution speed hit due to the use of a code interpreter in the PICAXE micro instead of using a compiler to generate machine code for a plain PIC. Again, I don't see this execution speed penalty as a major issue for most applications. As you gain experience you could make a switch to standard PIC micros and use C or assembly language. The group behind PICAXE (Revolution Education in Britain) gets funds from selling the PICAXE versions of the PIC micro (preloaded with the program loader and interpreter) and development boards/kits. Here is a link to the free software development environment: http://www.picaxe.com/Software/PICAXE/PICAXE-Programming-Editor You can find more PICAXE info at (including lots of examples and tutorials): http://www.picaxe.com/ and there are three U.S. distributers: http://www.sparkfun.com/categories/125 http://www.robotshop.com/search/search.aspx?locale=en_us&keywords=picaxe http://www.phanderson.com/picaxe/ I/O Configuration - In parallel with a need for easy software development I see a need for easy configuration of I/O interfaces to the devices outside the module. There a plenty of examples and tutorials for interfacing the PICAXE to all types of devices and here are some examples of general purpose modules that allow I/O configuration (usually through the provision of a prototyping area on the module): >From VX-Aviation, the Proton-225 board based on a PIC micro with a prototyping area and a package using standard d-sub 25 pin connectors and housing which is compatible with the other products they provide. You can download a pdf description here: http://www.vx-aviation.com/docs.html >From PICAXE there are several standard development boards that include the provision for varying levels of I/O configuration: http://www.picaxe.com/Hardware/Project-Boards/PICAXE-08-Proto-Board/ http://www.picaxe.com/Hardware/Project-Boards/PICAXE-14-Project-Board/ http://www.picaxe.com/Hardware/Project-Boards/PICAXE-18-Project-Board/ I don't know enough about hardware design to know if the use of these types of boards or even just a prototyping board from Radio Shack are robust enough to handle the environment of mounting in an experimental aircraft but based on the VX-Aviation module it would seem they may be up to the job... Anyway, this note is getting a little long so I will end it here. I would appreciate feedback from anyone who is interested in something along these lines in order to see if my thoughts on this make any sense to anyone beside me. I am only interested as an end user of the module and have no real interest in designing / producing any type of hardware boards. I can handle setting up the I/O circuits on a pre-made board but I don't have much interest in board development even though I know it is something that is not that hard to learn. Just a matter of only so many things that you can do, even when you are retired from a "real" job. I have read and studied the AeroElectric Connection book and have a draft design for the electrical system on the Sonex Xenos motor glider that I am building. But as I pointed out in a previous note, like most software engineers, I know just enough about hardware design to be dangerous... Greg McHugh Read this topic online here: http://forums.matronics.com/viewtopic.php?p=370376#370376


    Message 10


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    Time: 09:58:33 AM PST US
    Subject: Re: Next generation wig-wag controller for LED
    lamps
    From: Daniel Hooper <enginerdy@gmail.com>
    To that goal, I'd like to suggest using an Arduino. The IDE is totally cross-platform, the programming language is C with some extra libraries, and the only difference between an Arduino and a plain Atmel AVR micro is the (free) boot loader, giving folks their choice of Arduino or AVR Studio. Additionally there is tons of forum support for programming those guys. I recently used one in a project where one of the goals was that it needed to be maintained by a moderately savvy high-school student. I think it's great for that kind of thing. Daniel On Apr 9, 2012, at 11:21 AM, "gregmchugh" <gregmchugh@aol.com> wrote: > To be useful for a wide audience there needs to be simple learning curve for developing the software > functionality and I/O configuration. I agree that the use of a PIC micro would be the way to go based on > their ready availability, good price per performance, and availability of development tools.


    Message 11


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    Time: 10:50:36 AM PST US
    Subject: Re: Next generation wig-wag controller for LED lamps
    From: "gregmchugh" <gregmchugh@aol.com>
    Daniel, I agree that the Arduino is a good option but, as I noted in another note which seems to be appearing under a different thread, I would be concerned that the learning curve for software development on an Arduino might be too steep for many potential users. I suggested the PICAXE micro as a good choice due to the simple learning curve. Both are viable options but they would seem to be to be targeted at slightly different users. The Arduino development environment makes learning to use the C language easier than many other options but it is still a language that takes significant learning to understand what the code is doing. This issue is not as significant as most C development environments, Arduino does ease the learning curve with a nice development environment and lots of tutorials and examples. I can see people starting out with PICAXE and moving to Arduino as they develop more complex applications. For people ready to tackle the added complexity of the software, Arduino is probably the best option. It is good that many options exist... Greg McHugh Read this topic online here: http://forums.matronics.com/viewtopic.php?p=370381#370381


    Message 12


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    Time: 10:50:36 AM PST US
    From: Paul Millner <millner@me.com>
    Subject: Who got lost without an ELT?
    >> Congresscritter disappeared in his light plane in Alaska Hale Boggs, whose daughter you've probably heard on the radio, Cokie Roberts... Paul -- Please note my new email address! millner@me.com


    Message 13


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    Time: 11:25:17 AM PST US
    From: "Robert L. Nuckolls, III" <nuckolls.bob@aeroelectric.com>
    Subject: Open source product development for OBAM aircraft
    At 11:21 AM 4/9/2012, you wrote: Bob, I probably should have changed the Subject line on this but I decided to leave it alone to continue the thread we had started. It is getting away from the LED wig-wag topic... Okay, how about 'open source product development for OBAM aircraft" I have thought about this a little and I think it would be worthwhile to consider the option of a general purpose programmable module and use the LED wig-wag as a simple example application. I see three useful characteristics for this module 1. Functionality set in software 2. Some capability to configure the I/O circuits for each application 3. A standard module package and connector such as the one you showed using an enclosed case with d-sub connector That was the idea behind the "do allot" ECB and companion schematic. It's readily deduced that no single product would use ALL the parts in the schematic. But selective use of parts and software offers a host of possibilities. This particular board was bounded by the dimensions of the case . . . but there are larger cases that could be considered. But there's value in maximizing the 'core' of a bill of materials that varies only slightly from product to product and this size seemed like a good starting place. To be useful for a wide audience there needs to be simple learning curve for developing the software functionality and I/O configuration. I agree that the use of a PIC micro would be the way to go based on their ready availability, good price per performance, and availability of development tools. <snip> My father-in-law has been doing my PIC software on a PICkit 1. I think they're $36 from Digikey. The source editor/compiler is free. http://tinyurl.com/7dq97tv <snip> I don't know enough about hardware design to know if the use of these types of boards or even just a prototyping board from Radio Shack are robust enough to handle the environment of mounting in an experimental aircraft but based on the VX-Aviation module it would seem they may be up to the job... these same considerations drove the do-lots board. Everything needed to do a lot of tasks could be completely contained in the 'standard enclosure'. Anyway, this note is getting a little long so I will end it here. I would appreciate feedback from anyone who is interested in something along these lines in order to see if my thoughts on this make any sense to anyone beside me. I am only interested as an end user of the module and have no real interest in designing / producing any type of hardware boards. I can handle setting up the I/O circuits on a pre-made board but I don't have much interest in board development even though I know it is something that is not that hard to learn. Not 'hard' but certainly time consuming. This is where the open-source approach might allow the community of interested users to contribute in concert with their interests and available time. For my part, I can readily advise on schematics and functionality that are 'aviation friendly'. Been doing that for decades. I would proposed that the development chain of any single device be published, certainly here on the List and perhaps archived on aeroelectric.com I did the c-mos gate wig-wag as a practical exercise with low risk for success. It's not been laid up on a board but could be easily brass-boarded and hardened for installation on an airplane. Doing a PIC based flasher might be the short path to success. The board and packaging is done. The aviation friendly architecture is done. So, tell you what. If you program this beastie, I'll supply the parts. We can turn this into a practical path to service your needs along with a teaching moment for interested readers. I'll turn it into an off-the-shelf product. I'll make cases and bare board available to anyone who wants to do their own version of a do-lots module. If they contribute their own efforts to the open-source library, then depending on interest-at-large . . . we can make that an off the shelf product as well. I'll look into the options for getting some beefier fets in the box. Bob . . .


    Message 14


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    Time: 11:38:11 AM PST US
    From: "Robert L. Nuckolls, III" <nuckolls.bob@aeroelectric.com>
    Subject: Re: ELT Antenna Mount
    Folks, It seems were getting a lot of ancillary issues injected to the conversation. With respect to the original question, installing the antenna in this manner is guaranteed to offer a substantial reduction of the system's ability to function. The relative effectiveness of emergency locator beacons took a 1000-fold jump when the technology added a GPS location tag to the ELT output. The over-all effectiveness is still limited by logistics. When minutes count, help is only hours away. Nonetheless, out of tens of thousands of ELT systems- installed, a few will be part of the post accident scenario. Fewer still will be credited with causing a happy ending. The regulatory matters surrounding ELT installations is only a symptom of the growing sphere of influence being exerted by an ever expanding cadre of regulators in all venues. All honorable citizens are encouraged to join the struggle to curtail such adventures. There are plenty of on-topic forums in which those pursuits can be exercised. Just not here. Bob . . .


    Message 15


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    Time: 12:20:48 PM PST US
    From: "Robert L. Nuckolls, III" <nuckolls.bob@aeroelectric.com>
    Subject: Re: Open source product development for OBAM aircraft
    At 11:57 AM 4/9/2012, you wrote: > >To that goal, I'd like to suggest using an Arduino. This is a highly capable device but a bit of an overkill for things like wig-wag flashers, voltage monitors, etc. The challenge is to exploit the scope of projects that can be implemented in a user friendly package of the smallest practical size, cost and parts count. An already stuffed Arduino board has no aviation friendly i/o or even an enclosure for $30. I would expect the wig-wag flasher to be drop-in ready for use on an airplane and have total bill of materials under $20 or so. Bob . . .


    Message 16


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    Time: 12:42:42 PM PST US
    Subject: Re: Open source product development for OBAM aircraft
    From: Daniel Hooper <enginerdy@gmail.com>
    That's true, but it's fairly simple to 'roll your own' Arduino with just an ATMega and a particular serial and reset schematic. I haven't done the design exercise, but an ATMega168 would probably do the job, and they're as little as $2.31 on Mouser. The FTDI serial chips are only $2 nowadays too, apparently, if you're inclined to make it USB programmable. There are definitely other solutions, but I've had a surprisingly good experience with these things. Daniel On Apr 9, 2012, at 2:19 PM, "Robert L. Nuckolls, III" <nuckolls.bob@aeroelectric.com> wrote: > > At 11:57 AM 4/9/2012, you wrote: >> >> To that goal, I'd like to suggest using an Arduino. > > This is a highly capable device but a bit of an > overkill for things like wig-wag flashers, voltage > monitors, etc. > > The challenge is to exploit the scope of > projects that can be implemented in a user > friendly package of the smallest practical > size, cost and parts count. An already stuffed > Arduino board has no aviation friendly i/o > or even an enclosure for $30. I would expect > the wig-wag flasher to be drop-in ready for > use on an airplane and have total bill of > materials under $20 or so. > > >


    Message 17


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    Time: 02:12:26 PM PST US
    From: "Robert L. Nuckolls, III" <nuckolls.bob@aeroelectric.com>
    Subject: Re: Open source product development for OBAM aircraft
    At 02:41 PM 4/9/2012, you wrote: > >That's true, but it's fairly simple to 'roll your own' Arduino with >just an ATMega and a particular serial and reset schematic. I >haven't done the design exercise, but an ATMega168 would probably do >the job, and they're as little as $2.31 on Mouser. >The FTDI serial chips are only $2 nowadays too, apparently, if >you're inclined to make it USB programmable. > >There are definitely other solutions, but I've had a surprisingly >good experience with these things. Sure . . . but the ATM168 is a big chip with lots of I/O we can't put into the enclosure I have. A large proportion of energy/time to bring a product to an airplane is packaging. If you can capitalize on off-the-shelf packaging, that problem goes away. If the ECB layout I have could be slightly modified to the new task, that time-to-market item is shortened. To be sure, there are MANY options capable of a host of tasks. I'll suggest we establish some design goals that get us to the finish line with a minimum of new investment. If we were talking about a product where projected sales were in the thousands or even hundreds, perhaps a 'next size up' enclosure with silicon capable of more expansion would be attractive. But I'd be surprised if construction/sales of the simplest and fastest project would exceed 100 pieces in the next 5 years. Return on investment of development time is much more significant for low volume projects. The PIC 12F675 is a reduced instruction set device usually programmed in assembler. This is an excellent learning environment for teaching micro-controllers and Bollean logic. It gets the student better connection with the inner workings of the chip. Bob . . .


    Message 18


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    Time: 02:15:09 PM PST US
    From: "Jeff Luckey" <JLuckey@pacbell.net>
    Subject: Open source product development for OBAM aircraft
    All Regarding Selection of Micro-controller: There should probably be some due diligence with respect to selection of micro-controller and micro-controller families to be considered for a Do-Lots (generic controller w/ hardened interfaces to the real world) device. I've used PIC & ATMEL uControllers and I have opinions about both (which I'm happy to share if people are interested). I'm hoping others on this list do too. With some careful design, it may be possible to create a device that is uController/Manufacturer agnostic. Food for thought... -Jeff Luckey -----Original Message----- From: owner-aeroelectric-list-server@matronics.com [mailto:owner-aeroelectric-list-server@matronics.com] On Behalf Of Robert L. Nuckolls, III Sent: Monday, April 09, 2012 10:24 Subject: AeroElectric-List: Open source product development for OBAM aircraft <nuckolls.bob@aeroelectric.com> At 11:21 AM 4/9/2012, you wrote: Bob, I probably should have changed the Subject line on this but I decided to leave it alone to continue the thread we had started. It is getting away from the LED wig-wag topic... Okay, how about 'open source product development for OBAM aircraft" I have thought about this a little and I think it would be worthwhile to consider the option of a general purpose programmable module and use the LED wig-wag as a simple example application. I see three useful characteristics for this module 1. Functionality set in software 2. Some capability to configure the I/O circuits for each application 3. A standard module package and connector such as the one you showed using an enclosed case with d-sub connector That was the idea behind the "do allot" ECB and companion schematic. It's readily deduced that no single product would use ALL the parts in the schematic. But selective use of parts and software offers a host of possibilities. This particular board was bounded by the dimensions of the case . . . but there are larger cases that could be considered. But there's value in maximizing the 'core' of a bill of materials that varies only slightly from product to product and this size seemed like a good starting place. To be useful for a wide audience there needs to be simple learning curve for developing the software functionality and I/O configuration. I agree that the use of a PIC micro would be the way to go based on their ready availability, good price per performance, and availability of development tools. <snip> My father-in-law has been doing my PIC software on a PICkit 1. I think they're $36 from Digikey. The source editor/compiler is free. http://tinyurl.com/7dq97tv <snip> I don't know enough about hardware design to know if the use of these types of boards or even just a prototyping board from Radio Shack are robust enough to handle the environment of mounting in an experimental aircraft but based on the VX-Aviation module it would seem they may be up to the job... these same considerations drove the do-lots board. Everything needed to do a lot of tasks could be completely contained in the 'standard enclosure'. Anyway, this note is getting a little long so I will end it here. I would appreciate feedback from anyone who is interested in something along these lines in order to see if my thoughts on this make any sense to anyone beside me. I am only interested as an end user of the module and have no real interest in designing / producing any type of hardware boards. I can handle setting up the I/O circuits on a pre-made board but I don't have much interest in board development even though I know it is something that is not that hard to learn. Not 'hard' but certainly time consuming. This is where the open-source approach might allow the community of interested users to contribute in concert with their interests and available time. For my part, I can readily advise on schematics and functionality that are 'aviation friendly'. Been doing that for decades. I would proposed that the development chain of any single device be published, certainly here on the List and perhaps archived on aeroelectric.com I did the c-mos gate wig-wag as a practical exercise with low risk for success. It's not been laid up on a board but could be easily brass-boarded and hardened for installation on an airplane. Doing a PIC based flasher might be the short path to success. The board and packaging is done. The aviation friendly architecture is done. So, tell you what. If you program this beastie, I'll supply the parts. We can turn this into a practical path to service your needs along with a teaching moment for interested readers. I'll turn it into an off-the-shelf product. I'll make cases and bare board available to anyone who wants to do their own version of a do-lots module. If they contribute their own efforts to the open-source library, then depending on interest-at-large . . . we can make that an off the shelf product as well. I'll look into the options for getting some beefier fets in the box. Bob . . .


    Message 19


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    Time: 03:40:29 PM PST US
    Subject: Re: Open source product development for OBAM aircraft
    From: "gregmchugh" <gregmchugh@aol.com>
    Bob, Sounds like a reasonable approach to me. Using these PIC chips gives a lot of options for software development. The kit you mention is $36 direct from Microchip. I just ordered one and will come up with the code for the wig-wag example using the kit. We just need to decide on which chip provides the right capabilities for the expected applications. I expect the option exists to allow several of the PIC chips to drop into the same board layout since the added pins simply increase the number of I/O ports. I believe the PICAXE chips are drop in replacements for the standard PIC chips supported by the kit you referenced without the need for the development kit. They can be programmed using the PICAXE kits which are readily available for $30 to $50 with the major cost being a USB programming cable. If you have a serial port available the cable is $6. I expect the serial cable is easy to make yourself since it is simply a connection to a 3.5mm stereo audio plug... Development tools for BASIC on the PICAXE are free and there is also an option to program the PICAXE directly from flowcharts using the Logicator tool ($15 tool). Enough options to satisfy most of the potential users... Greg McHugh Read this topic online here: http://forums.matronics.com/viewtopic.php?p=370402#370402


    Message 20


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    Time: 04:47:16 PM PST US
    Subject: Re: Open source product development for OBAM aircraft
    From: "gregmchugh" <gregmchugh@aol.com>
    Bob, One question I forgot to ask in the previous note. When I looked at using the Perihelion Wig-Wag for my LED landing lights I was surprised at the compact size and the capability to switch the loads on standard landing lights. Is there something unique about this design to handle the 250 watt load? Greg McHugh Read this topic online here: http://forums.matronics.com/viewtopic.php?p=370405#370405


    Message 21


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    Time: 07:41:32 PM PST US
    From: "Robert L. Nuckolls, III" <nuckolls.bob@aeroelectric.com>
    Subject: Re: Open source product development for OBAM
    aircraft At 06:45 PM 4/9/2012, you wrote: > >Bob, > >One question I forgot to ask in the previous note. When I looked at >using the Perihelion Wig-Wag for my LED landing lights I was >surprised at the compact size and the capability to switch the loads >on standard landing lights. Is there something unique about this >design to handle the 250 watt load? You'd have to check with Eric as to his design philosophy but based on what is generally known, getting the heat in the FETs under control has two components. (1) Thermal resistance from the silicon to the ambient. Like ohms in current flow, thermal resistance has a quotient most often stated in degrees C in rise per watt of power in the junction. (2) Keeping power dissipated at a minimum by selecting a FET with the lowest practical on-resistance in combination with a healthy overhead for rated voltage. Check out this array of 30 volt FETs. http://tinyurl.com/6vxhkxg Then let's select a 2.1 milliohm resistance at 4.5 volts of gate drive. Nice specs but it's a bare chip intended for installation by bonding into a hybrid device. Okay back up let's leave the resistance alone and select 20 volts where it says we'll find 153 devices to select from. Lets go over in the array and look at surface mount parts with leads (67 choices). The next thing we're interested in is size. Just for grins, hit the SO-8 package (34 choices). Notice that we have three power dissipation choices. Let's go peek at the single 3.5 watt device. That gives us the IRF7811 with an logic level drive on resistance of 14 milliohms. Now, with the proposed 45 watt devices, let's assume 5A max at minimum bus voltage so 5A(squared) x .014 ohms equals 350 milliwatts. Hmmm . . . not bad. Let's go get the detailed data at: http://tinyurl.com/6qpt9cf We see there that thermal resistance junction-to- leads is on the order of 20 degrees C per watt. .35 watts will give us a 7 degree C rise on the junction over the temperature of the board. Now here's where it gets a little sticky. Our board is epoxy glass with most of the copper removed and the whole thing is enclosed in a plastic case with no ventilation. What we don't know is the thermal resistance board to ambient wile boxed up in this case. I'll go measure it in the next few days. This is done by cutting a piece of copper clad the same footprint as the proposed board. Glue a power resistor and thermocouple to the board. Close it up in the plastic case. Dump some handy amount of power into the resistor, say 1 watt. Then see what the temperature reads after an hour or so. This will yield the best possible heat transfer situation for one of these FETS soldered to the board. I'm thinking the 7811 might do the job. They're stock at Digikey for 1.50 in small quantities. Since this is a plastic enclosure, we'll qualify to cabin environments so 40 to 50 C is about the upper test limits. Okay, just for grins let's see how a pair of SO-8 chips goes into the space previously occupied by three DIP4 chips and some do-lots components. Emacs! Well, lookee there. Not only is there plenty of room, we might even put one on top and the other on the bottom so as to leave room for leaving more copper on the board around the chip. This exercise in cut and try on a four-cornered envelope with the final confirmation or denial of choice being a full power test in the temperature chamber. I have one of those. http://tinyurl.com/7yrrhhq So fortunately, we have access to quite a bit of experience to drive the corners of the envelope toward the component of choice. I'm pretty sure we can get a 5A switcher in this enclosure with comfortable head room for power handling. So now your schematic looks something like this: Emacs! When we went from do-lots to wig-wag, it got a lot simpler. Two outputs driving power FETs, two inputs to control for three states of function (OFF/WW/ON). So, first cut at the design looks good. If you can make the silicon sing, dance and do dishes, I'd say we're 50% of the way to having a useful product that meets design goals and offers a user friendly envelope and wiring interface. Bob . . .


    Message 22


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    Time: 07:50:59 PM PST US
    From: "Robert L. Nuckolls, III" <nuckolls.bob@aeroelectric.com>
    Subject: Re: Open source product development for OBAM
    aircraft > >Enough options to satisfy most of the potential users... Exactly. For years I tried to find a crack into which I could drive a wedge for distributed processing. We had dozens of little black boxes for current sensing, time delays, logic, thermostats, etc that all used discrete components and were designed 30 to 40 years ago. I even demonstrated that I could make huge reductions in parts count with similar reductions in size and weight, plus take advantage of pick-n-place assembly. But as soon as I mentioned software, everyone turns white and runs out the door. It didn't matter how simple the software task might be, those-who-know-more-about-airplanes-than-we-do- in-Washington insisted on piles of paper and buckets of holy-water with DO-178 'certification' and configuration management. A device with $20 worth of parts to do some simple task could cost $100,000 to qualify. So much for modern marvels. Hence, anything software was farmed out in the form of "do-everything" flight and airframe management computers with a $10,000 bill of materials and a 10 million dollar cert program. What's more, when it didn't work right, we had somebody else to throw rocks at and then wait around with everyone camping on a work order. Now, you and I have a chance to show the guys at Beech/Raytheon/HBC how to do a responsible job of incorporating software with a distributed processing approach to black box development. Ought to be fun. Bob . . .


    Message 23


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    Time: 08:01:06 PM PST US
    From: "Bill Bradburry" <bbradburry@bellsouth.net>
    Subject: Point me in the right direction
    My strobes will not fire when they are plugged into the plane electrical system. They will fire if 12V from a power supply is hooked up to them. The schematic is basically: battery, to master solenoid, to fuse, to switch, to strobe power supply. Sometimes it will fire once and stop and sometimes it will fire 6-7 times and stop. I have continuity with the ground pin on the Molex power supply connector to aircraft ground. With the master on, I have 12V at the fuse, I have 12V incoming to the switch. With the master on and the strobe switch off, I have .65V after the switch. With the strobe switch on I have 12V after the switch. With the strobe switch on I have sometimes 12V, sometimes 10V, and sometimes 8V at the power pin in the connector going to the strobe power supply. At first I thought the switch was bad then that I have a loose connection somewhere after the switch. It doesn't seem reasonable that all this could have happened at the same time. The strobes were fine till I was not able to visit the plane for about 6 months. The problem happened when I returned and tried to power them up. I suppose the Molex connector pins could be loose but that doesn't explain the low voltage. I plan to move the wire from the strobe switch to the position light switch tomorrow to see if that helps. None of the other light switches have voltage after them with the switch off. Any suggestions? Bill B


    Message 24


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    Time: 09:17:56 PM PST US
    From: "Bruce" <BGray@glasair.org>
    Subject: Point me in the right direction
    Check the wire crimps on the molex connectors. Sounds like something is not airtight and corroded over time. Bruce WWW.Glasair.org -----Original Message----- From: owner-aeroelectric-list-server@matronics.com [mailto:owner-aeroelectric-list-server@matronics.com] On Behalf Of Bill Bradburry Sent: Monday, April 09, 2012 10:59 PM Subject: AeroElectric-List: Point me in the right direction <bbradburry@bellsouth.net> My strobes will not fire when they are plugged into the plane electrical system. They will fire if 12V from a power supply is hooked up to them. The schematic is basically: battery, to master solenoid, to fuse, to switch, to strobe power supply. Sometimes it will fire once and stop and sometimes it will fire 6-7 times and stop. I have continuity with the ground pin on the Molex power supply connector to aircraft ground. With the master on, I have 12V at the fuse, I have 12V incoming to the switch. With the master on and the strobe switch off, I have .65V after the switch. With the strobe switch on I have 12V after the switch. With the strobe switch on I have sometimes 12V, sometimes 10V, and sometimes 8V at the power pin in the connector going to the strobe power supply. At first I thought the switch was bad then that I have a loose connection somewhere after the switch. It doesn't seem reasonable that all this could have happened at the same time. The strobes were fine till I was not able to visit the plane for about 6 months. The problem happened when I returned and tried to power them up. I suppose the Molex connector pins could be loose but that doesn't explain the low voltage. I plan to move the wire from the strobe switch to the position light switch tomorrow to see if that helps. None of the other light switches have voltage after them with the switch off. Any suggestions? Bill B




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