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authorMarius Peter <marius.peter@tutanota.com>2022-04-05 19:59:23 +0200
committerMarius Peter <marius.peter@tutanota.com>2022-04-05 19:59:23 +0200
commit5782c7c067fcd2331e74de220d404f77b766e6c6 (patch)
tree9f17960c2a1962b2405651784d323b3fd8adf75f /wiki/aerospace
parentd798383d2f8509a4f42ff3b68375f66c543ab5ce (diff)
Lots of wiki reorg & new files!
Diffstat (limited to 'wiki/aerospace')
-rw-r--r--wiki/aerospace/communication-protocols/ARINC-429.org18
-rw-r--r--wiki/aerospace/communication-protocols/CAN-bus.html335
-rw-r--r--wiki/aerospace/communication-protocols/CAN-bus.org18
-rw-r--r--wiki/aerospace/designing-aircraft.org19
-rw-r--r--wiki/aerospace/index.org10
-rw-r--r--wiki/aerospace/index.org.bkp23
-rw-r--r--wiki/aerospace/standard/ARP4754.org36
-rw-r--r--wiki/aerospace/standard/DO-160.org108
-rw-r--r--wiki/aerospace/v-model.org42
9 files changed, 0 insertions, 609 deletions
diff --git a/wiki/aerospace/communication-protocols/ARINC-429.org b/wiki/aerospace/communication-protocols/ARINC-429.org
deleted file mode 100644
index 220e27d..0000000
--- a/wiki/aerospace/communication-protocols/ARINC-429.org
+++ /dev/null
@@ -1,18 +0,0 @@
-# -*- mode: org; -*-
-
-#+TITLE: ARINC 429
-#+SUBTITLE: Mark33 Digital Information Transfer System (DITS)
-#+AUTHOR: Marius Peter
-#+DATE: <2022-03-25 Fri>
-#+OPTIONS: toc:nil
-
-#+DESCRIPTION: The ARINC 429 avionics data bus.
-
-#+TOC: headlines 2
-
-
-#+begin_abstract
-The =ARINC 429= technical standard defines the physical and electrical
-interfaces of a two-wire data bus and a data protocol to support an
-aircraft's avionics local area network.
-#+end_abstract
diff --git a/wiki/aerospace/communication-protocols/CAN-bus.html b/wiki/aerospace/communication-protocols/CAN-bus.html
deleted file mode 100644
index d12b862..0000000
--- a/wiki/aerospace/communication-protocols/CAN-bus.html
+++ /dev/null
@@ -1,335 +0,0 @@
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-<meta name="viewport" content="width=device-width, initial-scale=1" />
-<title>CAN bus</title>
-<meta name="generator" content="Org mode" />
-<meta name="author" content="Marius Peter" />
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- pre.src-shell:before { content: 'Shell Script'; }
- pre.src-ebnf2ps:before { content: 'ebfn2ps'; }
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- in ob-*.el */
- pre.src-cpp:before { content: 'C++'; }
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- /* add a generic configuration mode; LaTeX export needs an additional
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- /*]]>*///-->
-// @license-end
-</script>
-</head>
-<body>
-<div id="content">
-<h1 class="title">CAN bus
-<br />
-<span class="subtitle">A robust vehicle bus to enable hostless microcontroller communication.</span>
-</h1>
-<div id="table-of-contents">
-<h2>Table of Contents</h2>
-<div id="text-table-of-contents">
-<ul>
-<li><a href="#org1795fae">1. Introduction</a></li>
-<li><a href="#org9671f8c">2. Main topics</a></li>
-</ul>
-</div>
-</div>
-
-
-<div class="abstract" id="orgf3fc46c">
-<p>
-ARP4754 is a guidance issued by SAE.
-</p>
-
-</div>
-
-
-<div id="outline-container-org1795fae" class="outline-2">
-<h2 id="org1795fae"><span class="section-number-2">1</span> Introduction</h2>
-<div class="outline-text-2" id="text-1">
-<p>
-<a href="https://www.sae.org/standards/content/arp4754a/">https://www.sae.org/standards/content/arp4754a/</a>
-</p>
-</div>
-</div>
-
-
-<div id="outline-container-org9671f8c" class="outline-2">
-<h2 id="org9671f8c"><span class="section-number-2">2</span> Main topics</h2>
-<div class="outline-text-2" id="text-2">
-<table border="2" cellspacing="0" cellpadding="6" rules="groups" frame="hsides">
-
-
-<colgroup>
-<col class="org-right" />
-
-<col class="org-left" />
-
-<col class="org-left" />
-</colgroup>
-<thead>
-<tr>
-<th scope="col" class="org-right">§</th>
-<th scope="col" class="org-left">Theme</th>
-<th scope="col" class="org-left">Description</th>
-</tr>
-</thead>
-<tbody>
-<tr>
-<td class="org-right">1</td>
-<td class="org-left">Development</td>
-<td class="org-left">&#xa0;</td>
-</tr>
-
-<tr>
-<td class="org-right">2</td>
-<td class="org-left">Safety</td>
-<td class="org-left">&#xa0;</td>
-</tr>
-
-<tr>
-<td class="org-right">3</td>
-<td class="org-left">Requirements mgmt.</td>
-<td class="org-left">&#xa0;</td>
-</tr>
-
-<tr>
-<td class="org-right">4</td>
-<td class="org-left">Validation</td>
-<td class="org-left">&#xa0;</td>
-</tr>
-
-<tr>
-<td class="org-right">5</td>
-<td class="org-left">Verification</td>
-<td class="org-left">&#xa0;</td>
-</tr>
-
-<tr>
-<td class="org-right">6</td>
-<td class="org-left">Configuration mgmt.</td>
-<td class="org-left">&#xa0;</td>
-</tr>
-
-<tr>
-<td class="org-right">7</td>
-<td class="org-left">Process assurance</td>
-<td class="org-left">&#xa0;</td>
-</tr>
-
-<tr>
-<td class="org-right">8</td>
-<td class="org-left">Certification</td>
-<td class="org-left">&#xa0;</td>
-</tr>
-</tbody>
-</table>
-</div>
-</div>
-</div>
-<div id="postamble" class="status">
-<p class="date">Date: 2022-03-25 Fri 00:00</p>
-<p class="author">Author: Marius Peter</p>
-<p class="date">Created: 2022-03-25 Fri 17:49</p>
-<p class="validation"><a href="https://validator.w3.org/check?uri=referer">Validate</a></p>
-</div>
-</body>
-</html>
diff --git a/wiki/aerospace/communication-protocols/CAN-bus.org b/wiki/aerospace/communication-protocols/CAN-bus.org
deleted file mode 100644
index 2abbd23..0000000
--- a/wiki/aerospace/communication-protocols/CAN-bus.org
+++ /dev/null
@@ -1,18 +0,0 @@
-# -*- mode: org; -*-
-
-#+TITLE: CAN bus
-#+SUBTITLE: A robust vehicle bus to enable hostless microcontroller communication.
-#+AUTHOR: Marius Peter
-#+DATE: <2022-03-25 Fri>
-#+OPTIONS: toc:nil
-
-#+DESCRIPTION: CAN bus: a robust vehicle bus to enable hostless microcontroller communication.
-
-#+TOC: headlines 2
-
-
-#+begin_abstract
-The CAN bus design solves several engineering challenges, namely how
-to minimize copper usage in vehicle microcontroller communication
-lines.
-#+end_abstract
diff --git a/wiki/aerospace/designing-aircraft.org b/wiki/aerospace/designing-aircraft.org
deleted file mode 100644
index a3ebb3d..0000000
--- a/wiki/aerospace/designing-aircraft.org
+++ /dev/null
@@ -1,19 +0,0 @@
-# -*- mode: org; -*-
-
-#+TITLE: Designing aircraft
-#+SUBTITLE: How does one design an aircraft?
-#+AUTHOR: Marius Peter
-#+DATE: <2022-03-01 Tue>
-#+EMAIL: mlnp@tuta.io
-#+OPTIONS: toc:nil
-
-#+DESCRIPTION: aircraft design tutorial
-#+KEYWORDS: aerospace design
-
-#+TOC: headlines 2
-
-
-#+begin_abstract
-The DO-160 document is a standard for environmental testing for
-airborne equipment published by the RTCA.
-#+end_abstract
diff --git a/wiki/aerospace/index.org b/wiki/aerospace/index.org
deleted file mode 100644
index 77a2482..0000000
--- a/wiki/aerospace/index.org
+++ /dev/null
@@ -1,10 +0,0 @@
-#+TITLE: Sitemap for project wiki---aerospace
-
-- [[file:designing-aircraft.org][Designing aircraft]]
-- [[file:v-model.org][V-model]]
-- communication-protocols
- - [[file:communication-protocols/ARINC-429.org][ARINC 429]]
- - [[file:communication-protocols/CAN-bus.org][CAN bus]]
-- standard
- - [[file:standard/ARP4754.org][ARP4754]]
- - [[file:standard/DO-160.org][DO-160]] \ No newline at end of file
diff --git a/wiki/aerospace/index.org.bkp b/wiki/aerospace/index.org.bkp
deleted file mode 100644
index e4c161e..0000000
--- a/wiki/aerospace/index.org.bkp
+++ /dev/null
@@ -1,23 +0,0 @@
-# -*- mode: org; -*-
-
-#+TITLE: Aerospace
-#+SUBTITLE: Various topics around aerospace engineering.
-#+AUTHOR: Marius Peter
-#+DATE: <2022-03-12 Sat>
-#+OPTIONS: toc:nil
-
-#+DESCRIPTION: Various topics around aerospace engineering.
-#+HTML_LINK_UP: ../index.html
-#+HTML_LINK_HOME: https://mlnp.fr
-
-
-#+begin_abstract
-Aerospace is amongst my main centers of interest, I am very fortunate
-to be able to work in this domain.
-#+end_abstract
-
-
-* Main pages
-
-- [[file:designing-aircraft.org][Designing Aircraft]]
-- [[file:v-model.org][The V-model]]
diff --git a/wiki/aerospace/standard/ARP4754.org b/wiki/aerospace/standard/ARP4754.org
deleted file mode 100644
index fa7a5e1..0000000
--- a/wiki/aerospace/standard/ARP4754.org
+++ /dev/null
@@ -1,36 +0,0 @@
-# -*- mode: org; -*-
-
-#+TITLE: ARP4754
-#+SUBTITLE: Guidelines For Development Of Civil Aircraft and Systems.
-#+AUTHOR: Marius Peter
-#+DATE: <2022-02-11 Fri>
-#+EMAIL: mlnp@tuta.io
-#+OPTIONS: toc:nil
-
-#+KEYWORDS: aerospace, SAE, ARP 4754
-
-#+TOC: headlines 2
-
-
-#+begin_abstract
-ARP4754 is a guidance issued by SAE.
-#+end_abstract
-
-
-* Introduction
-
- https://www.sae.org/standards/content/arp4754a/
-
-
-* Main topics
-
-| § | Theme | Description |
-|---+---------------------+-------------|
-| 1 | Development | |
-| 2 | Safety | |
-| 3 | Requirements mgmt. | |
-| 4 | Validation | |
-| 5 | Verification | |
-| 6 | Configuration mgmt. | |
-| 7 | Process assurance | |
-| 8 | Certification | |
diff --git a/wiki/aerospace/standard/DO-160.org b/wiki/aerospace/standard/DO-160.org
deleted file mode 100644
index ea6f19b..0000000
--- a/wiki/aerospace/standard/DO-160.org
+++ /dev/null
@@ -1,108 +0,0 @@
-# -*- mode: org; -*-
-
-#+TITLE: DO-160
-#+SUBTITLE: Environmental Conditions and Test Procedures for Airborne Equipment.
-#+AUTHOR: Marius Peter
-#+DATE: <2022-02-11 Fri>
-#+EMAIL: mlnp@tuta.io
-#+OPTIONS: toc:nil
-
-#+DESCRIPTION: Environmental Conditions and Test Procedures for Airborne Equipment.
-#+KEYWORDS: aerospace, rtca, DO-160
-
-
-#+TOC: headlines 2
-
-
-#+begin_abstract
-The DO-160 document is a standard for environmental testing for
-airborne equipment published by the RTCA.
-#+end_abstract
-
-
-* Introduction
-
- https://do160.org/rtca-do-160g/
-
-
-* Equipment categories
-
-Equipments are categorized as a function of the environments to which
-they are subjected during normal operation.
-
-
-* Sections
-
-Sections 7 and 8 are aircraft dependent.
-
-
-** List
-:PROPERTIES:
-:HTML_CONTAINER_CLASS: big-table
-:END:
-
-#+NAME: sections
-#+CAPTION: List of DO-160 section.
-| § | Name | Concerns the effects of... | Parameters of interest |
-|----+------------------------------------------+------------------------------------------------------------------------------------+----------------------------------------------------------------------------|
-| 1 | /Introductory sections/ | /N/A/ | /N/A/ |
-| 2 | | | |
-| 3 | | | |
-|----+------------------------------------------+------------------------------------------------------------------------------------+----------------------------------------------------------------------------|
-| 4 | Temperature | Temperature on the system. | Temperature, condensation. |
-|----+------------------------------------------+------------------------------------------------------------------------------------+----------------------------------------------------------------------------|
-| 4 | Altitude | Altitude & cabin depressurization on performance. | Dielectric strength, (rapidly) varying air pressure. |
-|----+------------------------------------------+------------------------------------------------------------------------------------+----------------------------------------------------------------------------|
-| 5 | Temperature Variation | Extreme temperature changes. | Temperature delta, thermal expansion coefficients. |
-|----+------------------------------------------+------------------------------------------------------------------------------------+----------------------------------------------------------------------------|
-| 6 | Humidity | High concentrations of humidity; ability to withstand moisture effects.[fn:1] | Hygrometry. |
-|----+------------------------------------------+------------------------------------------------------------------------------------+----------------------------------------------------------------------------|
-| 7 | Shock & Crash safety | Mechanical shock. Ensures the item does not become a projectile in a crash. | Potential for projectile behavior. |
-|----+------------------------------------------+------------------------------------------------------------------------------------+----------------------------------------------------------------------------|
-| 8 | Vibration | Vibrations. | Normal operation in all vibration scenarios. |
-|----+------------------------------------------+------------------------------------------------------------------------------------+----------------------------------------------------------------------------|
-| 9 | Explosion proofness | Vacuum + gaseous mixture of combustibles. | The unit must be operable without igniting the environment. |
-|----+------------------------------------------+------------------------------------------------------------------------------------+----------------------------------------------------------------------------|
-| 10 | Water proofness | Dripping water or pooled water. | Normal operation after exposure. |
-|----+------------------------------------------+------------------------------------------------------------------------------------+----------------------------------------------------------------------------|
-| 11 | Fluids susceptibility | Various fluids including carbonated sugared beverages and cleaners/solvents. | Normal operation after exposure. |
-|----+------------------------------------------+------------------------------------------------------------------------------------+----------------------------------------------------------------------------|
-| 12 | Sand & Dust | Blowing sand and dust of specific particle sizes. | Normal operation after exposure. |
-|----+------------------------------------------+------------------------------------------------------------------------------------+----------------------------------------------------------------------------|
-| 13 | Fungus Resistance | Fungi under conditions favorable for their development.[fn:3] | Fungal proliferation. |
-|----+------------------------------------------+------------------------------------------------------------------------------------+----------------------------------------------------------------------------|
-| 14 | Salt & Fog | Multiple exposures of salt fog and drying; environmentally accelerated corrosion. | Normal operation after exposure. |
-|----+------------------------------------------+------------------------------------------------------------------------------------+----------------------------------------------------------------------------|
-| 15 | Magnetic effect | Magnetic effects on the aircraft's compass. | Normal aircraft compass function. |
-|----+------------------------------------------+------------------------------------------------------------------------------------+----------------------------------------------------------------------------|
-| 16 | Power input | Input power emissions, susceptibility, transients, drop-outs, hold-up.[fn:2] | Voltage, current, phase. |
-|----+------------------------------------------+------------------------------------------------------------------------------------+----------------------------------------------------------------------------|
-| 17 | Voltage spike | Voltage spikes caused by input power. | AC/DC voltage. |
-|----+------------------------------------------+------------------------------------------------------------------------------------+----------------------------------------------------------------------------|
-| 18 | Audio Frequency Conducted Susceptibility | Frequency components during normal operation. | Power source harmonics. |
-|----+------------------------------------------+------------------------------------------------------------------------------------+----------------------------------------------------------------------------|
-| 19 | Induced Signal Susceptibility | Induced voltages in the equipment interconnect circuit configuration. | power frequency harmonics; audio frequency signals, electrical transients. |
-|----+------------------------------------------+------------------------------------------------------------------------------------+----------------------------------------------------------------------------|
-| 20 | RF emission and susceptibility | Normal operation on radio frequency emission energy and susceptibility. | |
-| 21 | | | |
-|----+------------------------------------------+------------------------------------------------------------------------------------+----------------------------------------------------------------------------|
-| 22 | Lightning susceptibility | Direct and indirect effects, depending on location. | induced transients in the airframe or wire bundle. |
-| 23 | | | |
-|----+------------------------------------------+------------------------------------------------------------------------------------+----------------------------------------------------------------------------|
-| 24 | Icing | Icing conditions arising from rapid changes in temperature, altitude and humidity. | Presence of ice. |
-|----+------------------------------------------+------------------------------------------------------------------------------------+----------------------------------------------------------------------------|
-| 25 | ESD | ESD in handling and operation. | ESD. |
-|----+------------------------------------------+------------------------------------------------------------------------------------+----------------------------------------------------------------------------|
-| 26 | Flammability | Normal operation on presenting a fire hazard. | Normal operation not causing a fire. |
-
-
-* Footnotes
-
-[fn:3] This includes high humidity, a warm atmosphere, and the
-presence of inorganic salts.
-
-[fn:2] Full flight mission must be considered, from prior to the
-engine start, to after landing---including emergencies.
-
-[fn:1] Moisture sensitive devices may experience issues with this test
-and require conformal coat or other types of protection.
diff --git a/wiki/aerospace/v-model.org b/wiki/aerospace/v-model.org
deleted file mode 100644
index 6addaca..0000000
--- a/wiki/aerospace/v-model.org
+++ /dev/null
@@ -1,42 +0,0 @@
-# -*- mode: org; -*-
-
-#+TITLE: V-model
-#+SUBTITLE: Guidelines For Development Of Civil Aircraft and Systems.
-#+AUTHOR: Marius Peter
-#+DATE: <2022-02-11 Fri>
-#+EMAIL: mlnp@tuta.io
-#+OPTIONS: toc:nil
-
-#+KEYWORDS: aerospace, systems, development, engineering, model
-
-#+TOC: headlines 2
-
-
-#+begin_abstract
-The V-model represents the lifecycle of a system's development.
-#+end_abstract
-
-
-* TODO Representation
-
-This is the graphical representation of the v-model.
-
-#+NAME: v-model
-#+BEGIN_SRC plantuml :file ../images/v-model.png :cache yes
- @startuml
- !theme cerulean-outline
- actor Operator as operational
- collections Functions as functional
- control Logic as logical
- boundary Physical as physical
-
- operational -> functional: Requirements
- functional -> logical: Specification
- logical -> physical: Build plan
- physical -> logical
- logical -> functional
- functional -> operational
-#+END_SRC
-
-#+RESULTS[7e1fc2faaeb214ca241c5b4126d06cab1818ac52]: v-model
-[[file:../images/v-model.png]]
Copyright 2019--2026 Marius PETER