[psas-avionics] GPS outage

2015-06-22 Thread I
To the GPS folks, there is an interesting event that will occur this week starting in 15 minutes or so, and going on sporadically this week/weekend. There is a planned GPS outage over a broad area detailed here: https://www.faasafety.gov/files/notices/2015/Jun/NSAWC_15-01_GPS_Flight_Advisory.pdf

Re: [psas-avionics] 2 minute hate on the MAX2769

2015-02-06 Thread I
ick your sample frequency to be at least 2 x (IF freq + 1 sided bandwidth). > > Anyone have anything to say about this? I'd appreciate thoughts on this! > Another possibility... Just use the 2 "I" bits at twice the sample frequency and do the I-Q split in software with t

Re: [psas-avionics] No Useful Data From Flight Computer

2013-07-05 Thread I
odule? > > On 07/04/2013 10:23 PM, Nathan Bergey wrote: > > There is no data from the launch (T-0 to apogee). The last logfile > > starts *after* we're already on parachutes. > > > > > > I suspect we rebooted on motor ignition. > > > __

Re: [psas-avionics] No Useful Data From Flight Computer

2013-07-05 Thread I
gt; > The raw logs are all here: > > https://github.com/psas/flight_data-launch10/tree/master/fc/fc > > > I finished writing a parser for the FCF logs tonight and found what I > suspected based on the few packets that made it to the ground: > > There is no data from the launc

Re: [psas-avionics] Fwd: [RE]Re: Your Atom FC and the PCM-3680i CAN card

2012-06-27 Thread I
cate,Datasheet,Driver,Firmware,Manual,Online%20Training,Specification,Utility,FAQ,Installation,Software%20API,Software%20API%20Manual>" then click Driver(3). They have Linux (your OS) and QNX (my OS). I don't remember if I tested them or not, but I'm sure they work. This card seems we

Re: [psas-avionics] GFE connection to the ADIS?

2012-05-12 Thread I
>"The open drain SPI option is not implemented in this design. When a > device >is set up to be a slave, its I/Os are only active when it is > selected by the >SSEL signal being active." > >Since we will run the ADIS with the LPC in master mode, I d

Re: [psas-avionics] Question about I/O register

2011-10-25 Thread I
On Tue, Oct 25, 2011 at 1:06 PM, Naga Pinjala wrote: > No, I meant for turning off that output latch. > Sorry, I'm lost. What are you trying to do? ___ psas-avionics mailing list psas-avionics@lists.psas.pdx.edu http://lists.psas.pdx.

Re: [psas-avionics] Question about I/O register

2011-10-25 Thread I
On Tue, Oct 25, 2011 at 9:37 AM, Nagasrinivas Pinjala wrote: > Dan's answer is bit cryptic and needs more explanation. I referred the > manual but it only speaks about how setting the bits in GPIO registers sets > or clears the corresponding pins. > > >>" The P

Re: [psas-avionics] Question about I/O register

2011-10-25 Thread I
I don't think that's correct. Bit 25 *will* be cleared, but the |= won't help. The 'SET' registers will only set the GPIO bits. I think they are always read back as '0', or at least they revert to '0' as soon as they have modified the output latch. Rea

Re: [psas-avionics] USB Isoc update

2010-09-18 Thread I
A couple of questions from someone familiar with real-time, distributed communication; but not with usb isoc... When you say 'read', are you describing the process that 1) requests information from a remote source, 2) waits for the reply, and then 3) returns that information to an applicati

Re: [psas-avionics] Help with the flight computer, and a real time Linux patch set

2010-02-26 Thread I
* bandwidth) as we proved when considering actuator force would destroy the fins, yet I think I can easily make the case that it must be faster than 10Hz (which is a 0.25-0.50Hz *control* bandwidth) due to the fast roll axis dynamics. So, between 10 and 1000 loops per second. If I had to

Re: [psas-avionics] Help with the flight computer, and a real time Linux patch set

2010-02-25 Thread I
at measure processor load (instant, min, max, running average) based on idle time. As you build the control system, you watch the metrics. I don't let systems into 1st production with more than 70% loading. The last one I did shipped at less than 20% loading (fairly simple system). If the

Re: [psas-avionics] Flight computers...

2009-12-06 Thread I
unting and peripherals more manageable. In general, it probably doesn't matter what we launch, as long as we launch *something*. I think we could make any of these work, just some may take years longer than others. Wow, that *IS* a nice module. And yeah, we're kinda stuck with launchi

Re: [psas-avionics] Digital filters

2009-11-02 Thread I
Thanks for the replies. I thought I would touch on all of them in one email to keep the reading shorter. It was suggested off the list that I consider a decimation filter to downsample the sample rate. This sounds reasonable, but I implemented the iir filter at a 100 Hz sample rate and

[psas-avionics] Digital filters

2009-11-02 Thread I
y calculation (float-doubles), the DC offset is too big to make the filter useful when converted to fixed point math. 4) The fixed point data sizes get kind-of big for such a simple filter (long long) if I want to keep my resolution. 5) Filter coefficients for a 1000Hz sample rate and a 1Hz

[psas-avionics] IMU parts

2009-09-07 Thread I
Andrew and Tim, I'm working up a schematic for an IMU and I have a couple of questions you might be able to answer... First, Analog devices finally came out with a 3 axis accelerometer with decent range (8/2009). The ADXL326 has 3 axis +-16 g's. Noise spec is comparable but a

[psas-avionics] Analog to digital conversion

2009-07-30 Thread I
While investigating some analog to digital converters for an IMU project I'm working on, I settled on a TI ADS1278. One reason for using this ADC is that it has such fine resolution that I may be able to eliminate the amplifiers on the input for most inertial sensors! This AD

[psas-avionics] Liquid fueled rocket engines

2009-07-11 Thread I
Just as an FYI, I checked the rules for the BALLS launch regarding the use of a kerosene - nitrous oxide rocket motor after our discussion on Tuesday: "...Liquid Engines MUST request written approval from the Tripoli Board of Directors." They don't say they are illegal,

Re: [psas-avionics] [PSAS] Flight data from today's PSAS adventures

2009-06-01 Thread I
That was the motor chuffing, we think. Yeah, I don't think it's possible to hear a sonic boom if you can already hear the engine (though the chuff sound was impressive). My understanding is that a sonic 'boom' comes from the fact that you hear no sound, then all

Re: [psas-avionics] min trace width

2009-05-19 Thread I
/category/calculators/pcb/ look down the list. There are other handy calcs for power dissipation as well. For the second one, Check with your PCB Fab house and see what they are capable of doing. I generally add a little insurance by *not* going all the way down to the minimum trace/space

Re: [psas-avionics] LPC2368 and node5 design

2009-04-15 Thread I
Quoting Ken Zig : I am currently working on the EAGLE node 5 front end schematic and have a few questions. So far I have removed the portions of the SPS that I do not want to use.  I have inserted some of the new SPS design, and I have inserted the new LPC2368 controller. I have not

Re: [psas-avionics] LPC2368 package design

2009-04-13 Thread I
Here's a handy document I found when digging around the NXP website: http://www.nxp.com/acrobat_download/packages/footprint/FOOTPRINT-HTQFP-HLQFP-LQFP-REFLOW.pdf It gives the layout as recommended by NXP. Note that the thermal pads in the center of the layout are for the HTQ packages onl

Re: [psas-avionics] Pressure Sensor Test?

2009-02-05 Thread I
I have an exam Wednesday, so I won't be available until Thursday. As for times, the later the better, but 5:00 will likely work for me. Let's just use my code and my board. It just "works", and that's what we need. We need a way to get power into the chamber, and

Re: [psas-avionics] CAN on the MPC5200 FC: T-3 weeks until a no-go.

2009-02-02 Thread I
solate the host controller from the rest of the system.) Because CAN is a hard-wired bus, there's no physical-layer isolation between nodes, so a bus short means we're totally screwed, and a bus open means we're pretty well screwed, and a transceiver electrical failure could in principle

Re: [psas-avionics] CAN on the MPC5200 FC: T-3 weeks until a no-go.

2009-02-02 Thread I
ssible, either are trivial. It seemed to me like this particular feature was a pain when we tried this before? I thought we ended up kludging a node addressing scheme that borrowed bits that may or may not have belonged to us in order to get enough node addresses, and then had trouble getting thi

Re: [psas-avionics] CAN on the MPC5200 FC: T-3 weeks until a no-go.

2009-02-01 Thread I
Here we go again... if(OS != Linux) CAN = Easy; In one respect, I agree with Sarah's statement in that the only active node in an FC failure is the recovery node. Nothing else really matters. That said, if you *must* have some sort of non-usb back channel communication, CAN is the w

Re: [psas-avionics] Introducing the "Universal Rocket Bus"!

2009-01-18 Thread I
hen a signal is coming in? Collisions? Error checking? Seriously, I can't imagine it would take Dave and I more than a day to get CAN working on the TQM5200 once the toolchain is set up. Since no-one has actually completed any of the other node designs, using the LPC2368/78 has no aff

Re: [psas-avionics] Final review of cc1111-based flight computer.

2008-12-24 Thread I
Quoting Bdale Garbee : ARGH! Yes. Thank you for spotting that. No problem... About 2.2 nC at our operating point. ... I don't think it's necessary. But after talking to Keith, we'll add the footprints. We've got the space and I've got to rework that part of

Re: [psas-avionics] Final review of cc1111-based flight computer.

2008-12-23 Thread I
Quoting Andrew Greenberg : Hey Keith! Bdale and I spent the day reviewing chip foot prints and have quite a few minor updates. Bdale stuck them all on his server: http://www.gag.com/~bdale/tmp/telemetrum/ This directory has postscript versions of the schematic and the pc board along with

Re: [psas-avionics] Avionics toys arrived!

2008-06-30 Thread I
I've tested both of the ATV transmitters and cameras, and both work well. I have a couple of minutes of really cool video taken from an RC helicopter using the system, but it's saved to a mini DV tape. Anyone have a good way to get it off of the mini DV tape into an MPEG format?

Re: [psas-avionics] LPC-P2148 dev board from Sparkfun, lsp21isp, toolchain and wiggler jtag

2008-01-28 Thread I
I'll add my $0.02 here... I used Flash Magic (to get started) on the LPC -2378 board. It uses the serial connection to the ISP at up to 115200 bps (reasonably fast). It's free at http://www.flashmagictool.com (if you are running under windows). Anyway, it's a simple way