3 This is a recording dual-deploy altimeter for high power model rocketry
4 with integrated GPS and telemetry link.
6 These are photos of our current version,
7 which includes an integrated GPS receiver and patch antenna:
9 <a href="v0.2/cimg5164-cropped.jpg"> <img src="v0.2/cimg5164-thumb.jpg"></a>
10 <a href="v0.2/cimg5171-cropped.jpg"> <img src="v0.2/cimg5171-thumb.jpg"></a>
12 And this is a photo of our original board with serial port for off-board GPS,
13 without the big off-board 1000uF cap from the original ejection circuit:
15 <a href="v0.1/loadedpair.jpg"> <img src="v0.1/loadedpair-thumb.jpg"></a>
19 Bdale and Keith both own
20 [BeeLine](http://www.bigredbee.com/BeeLine.htm)
22 [Big Red Bee](http://www.bigredbee.com), and are pretty happy with them.
23 They use a PIC processor and a TI CC1050 transmitter chip, and
24 operate in the ham radio 70cm band.
26 One weekend while attending a conference together, we got to wondering if
27 we couldn't adapt one to use as a downlink for the
28 [AltusMetrum](../AltusMetrum/) altimeter board in addition to direction
29 finding after flight. That caused us to start thinking about other things
30 in the design we might want to tweak, and before long we were working on the
31 design of a new tracker board derived from the BeeLine design.
32 Another friend at the same conference showed us a board he was working on
33 using a different part in the same TI series, that integrated a transceiver
34 and CPU on the same chip.
35 It didn't take us long to realize that with such a part we could combine and
36 simplify things by building a new altimeter with integrated RF link! And
37 after gaining some experience in 2009 with a first version, we realized we
38 always want GPS on board, which lead to our current second generation boards.
44 * Recording altimeter for model rocketry
45 * Supports dual deployment (can fire 2 ejection charges)
46 * 70cm ham-band transceiver for telemetry downlink
47 * Barometric pressure sensor good to 45k feet MSL
48 * 1-axis high-g accelerometer for motor characterization
49 * SkyTraq Venus GPS module
50 * On-board non-volatile memory for flight data storage
51 * USB for power, configuration, and data recovery
52 * Integrated support for LiPo rechargeable batteries
53 * Uses LiPo to fire e-matches, optional support for separate pyro battery
54 * 2.75 x 1 inch board designed to fit inside 29mm airframe coupler tube
56 ### Developer View ###
58 * [TI CC1111F32](http://focus.ti.com/docs/prod/folders/print/cc1111f32.html) Low Power RF System-on-Chip
59 * Sub-1Ghz transceiver
64 * 6 12-bit analog inputs (11 bits with single-ended sensors)
65 * 2 channels of serial I/O
67 * [Atmel AT45DB081D](http://www.atmel.com/dyn/products/product_card.asp?part_id=3819) DataFlash memory
71 * other parts in this Atmel DataFlash series can optionally be used
73 * [Freescale MP3H6115A](http://www.freescale.com/webapp/search.partparamdetail.framework?PART_NUMBER=MP3H6115A6U) pressure sensor
74 * [Freescale MMA2202EG](http://www.freescale.com/webapp/search.partparamdetail.framework?PART_NUMBER=MMA2202EG) 50g accelerometer. Can use 40-200g variants!
76 * Written mostly in C with some 8051 assembler
77 * Runs from on-chip flash, uses on-chip RAM, stores flight data to
79 * USB serial emulation for "console" interface
81 * [gEDA](http://www.gpleda.org/) for schematic capture and PCB layout
82 * [SDCC](http://sdcc.sourceforge.net/) compiler and source debugger
84 * The hardware is licensed under the [TAPR](http://www.tapr.org) [Open Hardware License](http://www.tapr.org/ohl.html)
85 * The software is licensed [GPL version 2](http://www.gnu.org/licenses/old-licenses/gpl-2.0.html)
87 ### v0.1 Differences ###
89 * 2.5 x 1 inch board with all parts mounted on one side
90 * 4-pin PicoBlade serial port connector for attachment of external GPS module
91 * USB connector projected approximately 3mm over the edge of the board
92 * Debug connector used 4 IC socket pins on 100 mil centers
93 * no companion board interface
94 * [Microchip 25LC1024](http://www.microchip.com/wwwproducts/Devices.aspx?dDocName=en520389) CMOS serial EEPROM instead of DataFlash
97 * [Microchip MCP9700A](http://www.microchip.com/wwwproducts/Devices.aspx?dDocName=en027103) temperature sensor instead of using cc1111 on-chip sensor
98 * used 1000uF electrolytic capacitor charged to 5V for pyro charges
100 ## [Production History](production) ##
102 ## [Flight Logs](flightlogs) ##
106 * The CC1111F32 is a 36-pin QFN package, which necessitates reflow
107 soldering. Since we needed to reflow solder anyway, and because TI used
108 them in their reference design, we went a little crazy and used 0402
109 passive parts everywhere. That means working under a microscope to
110 place parts! Without an inspection microscope, loading and testing these
111 boards might be impossible.
113 * The v0.1 artwork has the USB connector footprint placed wrong, so that the
114 connector hangs out over the edge of the board instead of being flush with
117 * The v0.1 artwork has two issues that require cuts and jumps. The first is
118 that we need chip select on the SPI memory. To fix that, we give up the
119 ability to put the accelerometer into self-test mode and use that GPIO line
120 to pull chip select on the memory. The second is that the igniter sense
121 circuits each need a second resistor to complete the voltage divider so our
122 3.3V CPU ADC can read the 5V ejection voltage. This is fixed by changing
123 two resistor values, and tacking two additional resistors onto the board
124 with jumpers to ground.
128 The hardware design current gEDA files are available from
129 [git.gag.com](http://git.gag.com) in the project
130 [hw/telemetrum](http://git.gag.com/?p=hw/telemetrum;a=summary).
132 Work on the next version proceeds on the master branch, with occasional
133 temporary branches created when Bdale is making some major / speculative
134 change. The 'v0.2' and 'v0.1' branches document what we're actually flying
135 right now on the two respective PCB revisions. The 'ground' branch has a
136 cut-down schematic used to generate the BOM for partially loading v0.1 boards
137 to used on the ground. We call the on-the-ground version 'TeleDongle'.
139 For those who don't have ready access to the gEDA suite, here are pdf snapshots
140 of files in more easily readable form.
142 * These are from the v0.2 branch:
143 * [schematic](v0.2/telemetrum.pdf)
144 * [pcb artwork](v0.2/telemetrum.pcb.pdf)
145 * [bill of materials](v0.2/partslist.csv)
146 * These are as of the working-v0.1 tag:
147 * [schematic](v0.1/telemetrum.pdf)
148 * [pcb artwork](v0.1/telemetrum.pcb.pdf)
149 * [bill of materials](v0.1/telemetrum.bom)
151 Our [AltOS](../AltOS) firmware works well enough that we now routinely fly
152 TeleMetrum with no backup. Rockets with v0.1 boards have exceeded 50g
153 acceleration, been above Mach 1, and reached altitudes greater
154 than 12k feet AGL with great results. Keith's ground station program
155 called ao-view logs telemetry to disk, displays current and max values for
156 key parameters during flight, and even includes voice synthesis
157 during the flight so that our eyes can stay on the rockets! We have post
158 flight analysis software that makes it easy to extract data from the board,
159 analyze it, and even generate KML files for viewing flights in GoogleEarth!
160 More details on the software, including full source code and pre-built packages
161 can be found on the [AltOS](../AltOS) page on this site.
165 As of early February 2010, three prototypes of v0.2 are done and working on
166 the bench. We hope to flight test them shortly, then arrange a production
167 run in time to make TeleMetrum available in assembled and tested form to
168 others in the rocketry hobby who have expressed interest in time for the
171 Because we understand that not everyone uses Linux, we've started discussing
172 the best way to make a cross-platform ground station program for use with
173 [AltOS](../AltOS), perhaps in Java...