Page locked

This page is currently locked for editing by another user. You have to wait until this user finishes editing or the lock expires.

Currently locked by:
Lock expires at: 2026/02/01 09:14 (15 min)

You've loaded an old revision of the document! If you save it, you will create a new version with this data.

====== Automatic balloon launcher ABL01A ======

The whole system should serve as a complement to [[en:rmds|radio meteor detector]] network, and possibly to its visual alternative (video observation ((e.g. [[http://cement.fireball.sk/|CEMeNt]] network)) and bolide camera).

The purpose of the device is to refine the accuracy of a dark trajectory estimate of a meteor through introducing corrections to the flow of air masses during the meteor's flight in the atmosphere. As a consequence the elliptical impact area of the meteor on Earth's surface should reduce.

Data on atmospheric currents will be acquired by a weather balloon deflated immediately after the detection of a bolide flyby through the atmosphere. The balloon launch site should be chosen automatically based on the meteor trajectory estimate and known coordinates of the balloon silos in the network.

An important part of the system is the fully robotized discharged station (balloon silo), enabling the discharge of balloon from known coordinates without human intervention. A by-product of such development will be a device capable of future automation of classical meteorological [[http://en.wikipedia.org/wiki/Radiosonde|radiosonde]] discharge.
  
===== Ground discharge box =====

The ground balloon network station would consist of compact box containing technology needed to discharge the balloon __sonde__. The device must be able to withstand (in order of several years) the standby mode and wait for the command to release the sonde.

==== Technical requirements ====

Most of the electronics is composed of [[http://www.mlab.cz/ |MLAB brick system]] modules.

=== Communication with the network of stations ===

* Ethernet - [[en:eth|ETH01A]] module
  * RS232 - [[en:rs232single|RS232SINGLE01A]]
  * GSM (for remote areas)

At the same time, an equipment for telemetry reception of signal from other discharged radiosondae (([[http://www.radiosonde.eu/]], [[http://www.radiosonda.sk/]] )) from other stations is necessary.

[[en:stm32f10xrxt|STM32F10xRxT01A]] module meets the aforementioned requirements.

=== Power supply ===

* local (stand-alone) - photovoltaic panel
  * mains supply (AC adapter + UPS)

=== Fault diagnostics ===

* Successful start control (balloon lift measurement) 
  * Temperature, gas filling pressure, medium flow into the balloon measurement
  * Moisture inside the box measurement (in the case of leakage and loss of waterproofness through lid puncture , etc.)

=== Meteorological data ===

* The basic meteorological variables (temperature, pressure, wind speed) necessary to evaluate the possibility of start would be acquired from the nearest [[en:programming_tasks#framework_pro_distribuovane_merici_projekty|meteorological node]]  or local [[en:aws|AWS01B]] station
  * Local GPS (station position and accurate time) -> start log. [[cs:gps|GPS01A]]

==== Mechanical construction ====

The ground discharge box is constructed to be able to run under various weather conditions. It has a shape of triangular prism with one side standing on a raised platform and the other two covered with photovoltaic cells supplying energy to the electronics. After the discharge, they can be used to check the correct slide-down of the roof panels. The monitoring of the supplied power during the day also enables to check for the occurrence of solid obstacles in the vicinity of the station.

The material used for construction is welded polyethylene, making the station waterproof and resistant to dirt entry, that could damage the balloon.
 
  * A construction designed to enable the discharge of present-day professional weather balloons. 
  * Activation of mechanical components by burning the plastic fiber
  * Sealing of the balloon by melting the its neck (after filling the balloon)
  * The roof panels held flexibly by a stretchable strap, ensuring the sealing of the roof ridge.

=== __Actuators__ ===

Most of the actuators should be designed with an emphasis on maximal reliability. Therefore, they would probably be springs with __burnable__ plastic fuses (silicon fiber or ribbon burned by a powerful resistor).[[en:nfet4x|NFET4X01B]] module can be used To switch the current to resistors.

== Pneumatics ==

Helium management in the box must be designed to prevent the loss of helium by diffusion through porous materials like plastics or rubber. The main inlet valve must therefore be made of metal and ideally placed directly on the neck of the bottle.

An interesting idea would be to make use of bernoulli efect, when a low-pressure gas, like chemically produced hydrogen, would be sucked inside by a flow of the compressed helium, similar to inflation of [[http://www.kickstarter.com/projects/1484284472/windcatcher-inflates-in-seconds-with-no-power-or-p|this air pad]].

=== Carrier gas ===

In the case of our functional prototype, we have experimented with compressed helium as a source gas for the balloon filling. Preferred option, in this case is the use of disposable cartridges with compressed helium. Such packed helium is however quite expensive (700 Kč/0,1m³) and hydrogen is probably not available in this form.

An interesting solution seems to involve a chemical reaction to produce hydrogen directly in the discharge box. Discovered in 2007, a reaction of gallium and aluminum alloy with water produces hydrogen without an extensive heat production (([[https://news.uns.purdue.edu/x/2007a/070515WoodallHydrogen.html|New process generates hydrogen from aluminum alloy to run engines, fuel cells]])).

The course of the reaction is demonstrated in [[http://www.youtube.com/watch?v=JasZ8V6LpbQ|this video]]. You can purchase the necessary metals here:

* Galium [[http://unimagnet.cz/746-Gallium-10-gramu.html|UNIMAGNET]]
  * Powdered aluminum [[http://www.praskovekovy.cz/index.php?option=com_virtuemart&page=shop.browse&category_id=23&Itemid=26|pkchemie]]

It would be then sufficient to dry the hydrogen produced by this method by cartridge with silicagel.

Another option is to decompose the [[http://en.wikipedia.org/wiki/Sodium_borohydride|Sodium_borohydride]] by a catalyst.

=== Firmware ===

* The ground station should have an option to reject the discharge in accordance with the configuration set by its owner.

To ensure the running of independent processes the use of [[http://www.chibios.org/dokuwiki/doku.php|ChibiOS/RT]] is a viable option.

=== Block diagram ===
{{:en:arm_scheme.png?400|}}

=== Sensors ===

* The sensor of helium filling temperature - could be used to measure the temperature decrease during the expansion of helium from the pressure vessel
  * Cover opening detection
  * Humidity measurement in the box
  * The measurement of the current through burnable fuses - the [[en:nfet4x|NFET4X01B]] module has an analog output for each channel
  * Meteostation [[en:aws|AWS01B]] for measurement of the basic meteorological variables 
  * [[en:gps|GPS01A]] - a time synchronisation, an absolute knowledge of the station position, the possibility to generate a DGPS correction
  * Balloon __drag__ measurement
  * Gas flow into the balloon (by an [[http://en.wikipedia.org/wiki/Orifice_plate|orifice plate]])

===== Weather balloon =====

A non-flying prototype of the balloon will be developed using [[http://www.mlab.cz/Server/GenIndex/GenIndex.php?lang=cs&path=/Modules|MLAB]] modules.

[[en:atmegatq32|ATmegaTQ3201A]], [[en:sdcard|SDcard01B]], [[et:gps|GPS01A]]

==== Technical specifications ====

GPS carried by the balloon should be kept in FIX state in order to avoid a delay while waiting for a fix. At the same time, there also exist doubts concerning the accuracy of the GPS in higher altitudes, where the deviation of the measured altitude from the actual one can reach hundreds of meters.

=== Communication (Telemetry data) ===

* The primary objective is the measurement of the speed and direction of a wind at know points.
  * GPS data at 10Hz, text output [[http://en.wikipedia.org/wiki/NMEA_0183|NMEA]]
  * Other variables (like temperature, pressure, etc.) are optional.
  * Radio and audio beacon (?questionable)
  * Radio transmission of the telemetry in 27-450 MHz band: the possibility of using an unlicensed bands (SVN: VO-R-16, VO-R-10).
  *  Radiomodules: [[http://www.artbrno.cz]], [[http://www.anaren.com]], [[http://www.ams.com/eng/Products/RF-Products/RF-Transceivers/AS3900|AMS]].

The GPS must by chosen to function correctly at higher altitudes as well.((Limited by the [[http://en.wikipedia.org/wiki/CoCom#Legacy|CoCom]] directive)).

=== Power supply during the flight ===

* [[http://en.wikipedia.org/wiki/Lithium_battery|Lithium battery]] (does not generate heat, minimum operating temperature is -60°C) 
  * __Magnesium__ battery (generates heat to keep the electronics warm) 
  * [[http://en.wikipedia.org/wiki/Silver-oxide_battery|Stříbro-oxidový článek]] (withstands lower operating temperatures and is environmentally friendly
  * Ideal for use would be [[https://www.youtube.com/watch?feature=player_embedded&v=OtM6XJlynkk|supercapacitors]]

The solution to the problem of low temperature at higher altitudes could involve the preheating of the balloon at startup.

=== Construction ===

* Balloon - [[http://en.wikipedia.org/wiki/Polyethylene|PE]] sack (packed in order to increase the lifetime - as rubber degrades over time) ((http://en.wikipedia.org/wiki/Project_Mogul)) [[http://ukhas.org.uk/guides:balloon_data| Standard weather balloons parameters]]
  *

* Možnost dálkového odpojení balónu od sondy (ukončení stoupání)
  * Prototyp plněný [[http://cs.wikipedia.org/wiki/Helium|heliem]], produkční zařízení vodíkem (Použití vodíku je kromě nižší ceny i ekologičtější - hélium uvolněné do atmosféry je vlivem slunečního větru nenávratně odváto do vesmíru. A vodík navíc lze vyrábět chemickou reakcí přímo během napeouštění sondy). 
  * Splnění požadavků na bezpečnost provozu (letovou, majetkovou a personální)

=== Firmware ===

* Záznam dat v gondole balónu -> mikroSD karta

=== Blokové schéma ===
{{:cs:schema_atmega1.png?400|}}

==== Legislativní požadavky ====

Pravidla pro lety volných balónů bez pilota jsou definovány v leteckých předpisech L-2 Pravidla létaní, dodatek 5 a R.

=== Kategorie balónu ===

Balón by měl spadat do kategorie B2, která je definována jako volný balón s objemem menším než 3,25 m^3, přičemž žádný z rozměrů balónu nepřekračuje 2 m. Rozměr 2 m je rozměr při jeho maximálním naplnění/roztažení.

=== Povolení vypuštění ===

Užitečné zatížení představují předměty a materiály, které by v případě střetu s letadlem mohly způsobit poškození letadla (zejména prskavky, svítící tyčinky, lámací světla, LED diody apod.) a jakékoliv zatížení o hmotnosti přesahující 0,1 kg. 
Vzhledem k této definici bude nutné mít pro provoz balónu povolení. Všechny informace ohledně letu (jako je datum, čas, místo vypuštění, užitečné zatížení atp.) musí být zveřejněny v Letecké informační příručce (AIP). Pro vypuštění ve zvláštních případech, jako je mimořádné pozorování, je potřeba upozornit prostřednictvím navigační výstrahy formou zprávy NOTAM, která se musí podat minimálně 24 hodin před vzletem balónu.

=== Materiály ===

Balón nesmí být plněn hořlavými a výbušnými plyny s výjimkou povolení ÚCL.
Omezení pro materiál antény ani baterií nejsou definovány. 
Materiál balónu také není definován, ale při použití balónu o vysoké svítivosti nebo zhotoveného z materiálů o velké světelné nebo radarové odrazivosti musí být oznámeno nejbližšímu stanovišti letových provozních služeb.
Materiál (lano, provázek) spojující balón se sondou nesmí vydržet větší sílu než 230N.

=== Dostup ===

Pro dostup nejsou omezení.

=== Místo vypuštění ===

Omezení se týká všech Zakázaných, Nebezpečných a Omezených prostorů, stejně jako dočasně aktivovaných prostorů v době jejich používaní, s výjimkou kdy tak povolí ÚCL nebo kdy je prostor vyhrazen pro let předmětného balónu. Provoz balónu blízko hranic a letišť je problematický, nedoporučuje se.

=== Řešení legislativních problémů ===

* Navrhnout bezpečnou sondu, která splní požadavky ÚCL na bezpečnost letu. 
  * Řídit stoupání a aktivně zabránit vzniku kolize. (Takový systém by mohl zároveň zjednodušit návrat sondy podobně jako zde http://www.youtube.com/watch?v=rpBnurznFio ) 
  * Autodestrukce při hrozící srážce.
===== Řídící systém sítě =====

Konfigurace a řízení sítě by mělo být zajištěno [[cs:programming_tasks&#framework_pro_distribuovane_merici_projekty|univerzálním frameworkem pro distribuovaná měření]].

Please fill all the letters into the box to prove you're human. T W M X᠎ S Please keep this field empty:

Edit summary

Note: By editing this page you agree to license your content under the following license: CC Attribution-Noncommercial-Share Alike 4.0 International