projects:eurus
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projects:eurus [2012/05/29 15:15] – jcoxon | projects:eurus [2013/07/22 17:16] (current) – jcoxon | ||
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* 70cm (434Mhz) Tracker - [[https:// | * 70cm (434Mhz) Tracker - [[https:// | ||
- | ===== Launch 1 ===== | + | ===== Launch 1 |
* Aim to launch 26/27 May 2012 - to test float capabilities | * Aim to launch 26/27 May 2012 - to test float capabilities | ||
* He 1600g Balloon | * He 1600g Balloon | ||
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==== Launch Day ==== | ==== Launch Day ==== | ||
- | Relatively easy launch from Lavenham, Suffolk - filled the balloon inside a barn allowing easy calculation of lift. In total had 500g of neck lift aiming for an ascent rate of 2m/s. Payload had a few last minute issues regarding powering up the radio thought to be related to the power switch, also I realised there was an error in the code which detected that we had passed -6.0 longitude to increased the radio power which needed to be fixed. | + | Relatively easy launch from Lavenham, Suffolk - filled the balloon inside a barn allowing easy calculation of lift. In total had 500g of neck lift aiming for an ascent rate of 2m/s. Payload had a few last minute issues regarding powering up the radio thought to be related to the power switch, also we realised there was an error in the code which detected that we had passed -6.0 longitude to increased the radio power which needed to be fixed. |
Launch was at 1603 with some gusts of wind requiring a running launch. It became clear that the radio/ | Launch was at 1603 with some gusts of wind requiring a running launch. It became clear that the radio/ | ||
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{{: | {{: | ||
- | Flight time was 19hours (until signal lost) | + | * Flight time was 19hours (until signal lost) |
- | Float time was 15 hours (between 34 and 36km) | + | |
==== Lessons ==== | ==== Lessons ==== | ||
* 4 radials | * 4 radials | ||
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* don't bother with higher power (killed setup) | * don't bother with higher power (killed setup) | ||
* integer lat/lon worked? | * integer lat/lon worked? | ||
- | | + | |
+ | ===== Eurus 2 ===== | ||
+ | |||
+ | ==== Aim ==== | ||
+ | |||
+ | Similar flight to Eurus 1 however to attempt to float at a lower altitude (25km) in an attempt to take advantage of the faster winds. | ||
+ | |||
+ | ==== Components ==== | ||
+ | | ||
+ | * Neck valve + controller micro | ||
+ | * Parachute | ||
+ | * 434Mhz Tracker (similar to Eurus 1) | ||
+ | * Based on uAva (Atmega328, Ublox 6, RFM22b) | ||
+ | * Running plan13 for predicting ISS paths | ||
+ | * Improved antenna | ||
+ | |||
+ | ==== Eurus 2 Payload ==== | ||
+ | * Based on a uAva board | ||
+ | * ATmega328 with arduino bootloader | ||
+ | * RFM22b | ||
+ | * Ublox MAX-6 GPS with chip antennna | ||
+ | * Running at 8Mhz 3.3v | ||
+ | * 1/4 Wave GP (4 radials) Antenna | ||
+ | * Mass = 211g | ||
+ | |||
+ | === Telemetry === | ||
+ | |||
+ | < | ||
+ | < | ||
+ | |||
+ | Code can be found here: [[https:// | ||
+ | |||
+ | The payload is setup to calculate the Az and El of the ISS in relation to the balloon and if it is in view it will send APRS messages. The payload however will not be carrying a capable radio to communicate with the ISS, partially as this is a high risk launch testing the new valve but also the ISS has changed its packet system from 2m to 70cm which makes it harder to get a relay. We'll still test the flight code as it may come in useful in the future. | ||
+ | |||
+ | Also the radio will be reset every 50 strings as well as the GPS being ' | ||
+ | |||
+ | ==== Eurus 3 ==== | ||
+ | |||
+ | * [[eurus: | ||
+ | * [[eurus: |
projects/eurus.1338304555.txt.gz · Last modified: 2012/05/29 15:15 by jcoxon