X-Git-Url: https://git.gag.com/?a=blobdiff_plain;f=TeleMetrum%2Findex.mdwn;h=dbd4912367cead8f0a9971f11b9d87e6a9277c47;hb=f27f431a032bed4af3dc523aa666fe06e5971a01;hp=81a1df8ecce1b3160229daa767be184f399009a1;hpb=149b38fdd2aa7602c1a08ebab3df38d79750d27b;p=web%2Faltusmetrum diff --git a/TeleMetrum/index.mdwn b/TeleMetrum/index.mdwn index 81a1df8..dbd4912 100644 --- a/TeleMetrum/index.mdwn +++ b/TeleMetrum/index.mdwn @@ -1,11 +1,30 @@ # TeleMetrum This is a recording dual-deploy altimeter for high power model rocketry -with integrated telemetry link. +with integrated GPS and telemetry link. - - - +Production units are available from the +[Garbee and Garbee](http://auric.gag.com) web store. + +These are photos of our current production version, which includes an +integrated GPS receiver with active patch antenna: + + + + +These are photos of our second version, which included the integrated Venus +GPS receiver, but with a passive patch antenna that turned out to have +disappointing performance due to our many PCB geometry constraints. It also +used a voltage regulator with less capacity which we felt was marginal for +supporting the companion boards we have planned: + + + + +And this is a photo of our original board with serial port for off-board GPS, +without the big off-board 1000uF cap from the original ejection circuit: + + ## Motivation ## @@ -26,7 +45,9 @@ Another friend at the same conference showed us a board he was working on using a different part in the same TI series, that integrated a transceiver and CPU on the same chip. It didn't take us long to realize that with such a part we could combine and -simplify things by building a new altimeter with integrated RF link! +simplify things by building a new altimeter with integrated RF link! And +after gaining some experience in 2009 with a first version, we realized we +always want GPS on board, which lead to our current second generation boards. ## Features ## @@ -36,36 +57,42 @@ simplify things by building a new altimeter with integrated RF link! * Supports dual deployment (can fire 2 ejection charges) * 70cm ham-band transceiver for telemetry downlink * Barometric pressure sensor good to 45k feet MSL -* Temperature sensor * 1-axis high-g accelerometer for motor characterization +* On-board, integrated GPS receiver * On-board non-volatile memory for flight data storage -* Serial port for attachment of GPS module * USB for power, configuration, and data recovery * Integrated support for LiPo rechargeable batteries -* 2.5 x 1 inch board designed to fit inside 29mm airframe coupler tube +* Uses LiPo to fire e-matches, optional support for separate pyro battery +* 2.75 x 1 inch board designed to fit inside 29mm airframe coupler tube ### Developer View ### -* [TI CC1111F32](http://focus.ti.com/docs/prod/folders/print/cc1111f32.html) Low Power RF System-on-Chip - * Sub-1Ghz transceiver - * 8051 MCU - * 32k Flash - * 4k RAM - * USB 2.0 - * 6 12-bit analog inputs (11 bits with single-ended sensors) - * 2 channels of serial I/O - * digital I/O -* [Microchip 25LC1024](http://www.microchip.com/wwwproducts/Devices.aspx?dDocName=en520389) CMOS serial EEPROM - * 128k x 8 - * SPI interface -* Various Sensors +* Hardware Features + * [TI CC1111F32](http://focus.ti.com/docs/prod/folders/print/cc1111f32.html) Low Power RF System-on-Chip + * Sub-1Ghz transceiver + * 8051 MCU + * 32k Flash + * 4k RAM + * USB 2.0 + * 6 12-bit analog inputs (11 bits with single-ended sensors) + * 2 channels of serial I/O + * digital I/O + * [Atmel AT45DB081D](http://www.atmel.com/dyn/products/product_card.asp?part_id=3819) DataFlash memory + * 1M x 8 + * 256 byte page size + * SPI interface + * other parts in this Atmel DataFlash series can optionally be used + * [SkyTraq](http://www.skytraq.com.tw/) Venus634FLPx GPS receiver + * on-board [Taoglas AP.17A.01](http://www.taoglas.com/antennas/GPS_Antennas/Internal_GPS_-_Active_Patch_Modules/) + single-stage active patch antenna + * U.FL connector with 3.3V DC can be re-purposed for optional external amplified antennas + * async serial interface * [Freescale MP3H6115A](http://www.freescale.com/webapp/search.partparamdetail.framework?PART_NUMBER=MP3H6115A6U) pressure sensor * [Freescale MMA2202EG](http://www.freescale.com/webapp/search.partparamdetail.framework?PART_NUMBER=MMA2202EG) 50g accelerometer. Can use 40-200g variants! - * [Microchip MCP9700A](http://www.microchip.com/wwwproducts/Devices.aspx?dDocName=en027103) temperature sensor -* Software Features (planned) +* Software Features * Written mostly in C with some 8051 assembler * Runs from on-chip flash, uses on-chip RAM, stores flight data to - serial EEPROM chip + serial DataFlash chip * USB serial emulation for "console" interface * Tools Used * [gEDA](http://www.gpleda.org/) for schematic capture and PCB layout @@ -74,7 +101,31 @@ simplify things by building a new altimeter with integrated RF link! * The hardware is licensed under the [TAPR](http://www.tapr.org) [Open Hardware License](http://www.tapr.org/ohl.html) * The software is licensed [GPL version 2](http://www.gnu.org/licenses/old-licenses/gpl-2.0.html) -## [Production History](production) ## +### v0.2 Differences ### + +* 100ma LDO regulator instead of the current 150ma part +* no C38 footprint +* different value for C36 reset capacitor + +### v0.1 Differences ### + +* 2.5 x 1 inch board with all parts mounted on one side +* 4-pin PicoBlade serial port connector for attachment of external GPS module +* USB connector projected approximately 3mm over the edge of the board +* Debug connector used 4 IC socket pins on 100 mil centers +* no companion board interface +* 50ma LDO regulator on early boards, later boards used a 100ma part +* [Microchip 25LC1024](http://www.microchip.com/wwwproducts/Devices.aspx?dDocName=en520389) CMOS serial EEPROM instead of DataFlash + * 128k x 8 + * SPI interface +* [Microchip MCP9700A](http://www.microchip.com/wwwproducts/Devices.aspx?dDocName=en027103) discrete temperature sensor +* used 1000uF electrolytic capacitor charged to 5V for pyro supply +* two LEDs instead of one attached to CPU + +The elimination of the discrete temperature sensor and second LED were +necessary to support the companion board interface added in v0.2. + +## [Production History](../production) ## ## [Flight Logs](flightlogs) ## @@ -87,43 +138,74 @@ simplify things by building a new altimeter with integrated RF link! place parts! Without an inspection microscope, loading and testing these boards might be impossible. -* The v0.1 artwork has the USB connector footprint placed wrong, so that the - connector hangs out over the edge of the board instead of being flush with - the edge. - -* The v0.1 artwork has two issues that require cuts and jumps. The first is - that we need chip select on the SPI memory. To fix that, we give up the - ability to put the accelerometer into self-test mode and use that GPIO line - to pull chip select on the memory. The second is that the igniter sense - circuits each need a second resistor to complete the voltage divider so our - 3.3V CPU ADC can read the 5V ejection voltage. This is fixed by changing - two resistor values, and tacking two additional resistors onto the board - with jumpers to ground. +* The addition of on-board GPS in v0.2 means that the total power consumption + can exceed the rate at which we draw power from the USB interface, + particularly when the GPS is in cold start mode. This means a battery must + be attached during operation, and also that the battery will only charge + effectively from USB when the board is turned off. + +* The v0.1 artwork had three issues, two of which required physical rework + on each board. All of these issues were fixed in v0.2. + + * The USB connector footprint was placed wrong, so that the + connector hung out over the edge of the board instead of being + flush. + * We needed chip select on the SPI memory. To fix that, we gave up the + ability to put the accelerometer into self-test mode and used that + GPIO line to pull chip select on the memory, which required two + cuts and two jumpers. + * The igniter sense circuits each needed a second resistor to + complete the voltage divider so our 3.3V CPU ADC could read the + 5V ejection voltage. This was fixed by changing two resistor + values, and tacking two additional resistors onto the board + with jumpers to ground. ## Artifacts ## The hardware design current gEDA files are available from -[git.gag.com](http://git.gag.com) in the project hw/telemetrum. The 'fab' -tag on the master branch reflects -the artwork as sent out for PCB fab. The 'loaded' tag on the master branch -indicates the parts Bdale loads for a functional board, but the schematic -does not reflect the cuts and jumps or added resistors. The 'nextcut' branch -is work towards our next PCB revision. The 'ground' branch has a cut-down -schematic used to generate the BOM for partially loading boards to use in -the matching [TeleTerra](../TeleTerra) ground station design. - -For those who don't have ready access to the gEDA suite, here are pdf snapshots -of files in more easily readable form. The schematic and BOM are from the -'nextcut' branch as of 20 April 2009, the artwork is of the v0.1 boards: +[git.gag.com](http://git.gag.com) in the project +[hw/telemetrum](http://git.gag.com/?p=hw/telemetrum;a=summary). -* [schematic](telemetrum.pdf) -* [pcb artwork](telemetrum.pcb.pdf) -* [bill of materials](telemetrum.bom) +Work on the next version proceeds on the master branch, with occasional +temporary branches created when Bdale is making some major / speculative +change. The 'v0.2' and 'v0.1' branches document what we're actually flying +right now on the two respective PCB revisions. The 'ground' branch has a +cut-down schematic used to generate the BOM for partially loading v0.1 boards +to used on the ground. We call the on-the-ground version 'TeleDongle'. - -Keith has working firmware that has now been flown once and successfully -collected flight data to apogee. The source is also available from -[git.gag.com](http://git.gag.com) in the project fw/altos. Not that actually -building these sources requires a modifified version of sdcc and a set of -helper utilities that we're not publishing since we hope to have the important -bits accepted upstream shortly. Watch this space for more details soon. +For those who don't have ready access to the gEDA suite, here are pdf snapshots +of files in more easily readable form. + +* Production PCB version v1.0: + * [schematic](v1.0/telemetrum.pdf) + * [pcb artwork](v1.0/telemetrum.pcb.pdf) + * [bill of materials](v1.0/partslist.csv) +* These are from the v0.2 branch: + * [schematic](v0.2/telemetrum.pdf) + * [pcb artwork](v0.2/telemetrum.pcb.pdf) + * [bill of materials](v0.2/partslist.csv) +* These are as of the working-v0.1 tag: + * [schematic](v0.1/telemetrum.pdf) + * [pcb artwork](v0.1/telemetrum.pcb.pdf) + * [bill of materials](v0.1/telemetrum.bom) + +Our [AltOS](../AltOS) firmware works well enough that we now routinely fly +TeleMetrum with no backup. Rockets with v0.1 boards have exceeded 50g +acceleration, been above Mach 1, and reached altitudes greater +than 12k feet AGL with great results. Keith's ground station program +called ao-view logs telemetry to disk, displays current and max values for +key parameters during flight, and even includes voice synthesis +during the flight so that our eyes can stay on the rockets! We have post +flight analysis software that makes it easy to extract data from the board, +analyze it, and even generate KML files for viewing flights in GoogleEarth! +More details on the software, including full source code and pre-built packages +can be found on the [AltOS](../AltOS) page on this site. + +## Future Plans ## + +As of May 2010, version v1.0 is available for sale from the +[Garbee and Garbee](http://auric.gag.com) web store. + +Because we understand that not everyone uses Linux, development of a new +cross-platform ground station program written in Java is underway for use with +[AltOS](../AltOS).