From 5782c7c067fcd2331e74de220d404f77b766e6c6 Mon Sep 17 00:00:00 2001 From: Marius Peter Date: Tue, 5 Apr 2022 19:59:23 +0200 Subject: Lots of wiki reorg & new files! --- .../communication-protocols/ARINC-429.org | 18 -- .../aerospace/communication-protocols/CAN-bus.html | 335 --------------------- wiki/aerospace/communication-protocols/CAN-bus.org | 18 -- wiki/aerospace/designing-aircraft.org | 19 -- wiki/aerospace/index.org | 10 - wiki/aerospace/index.org.bkp | 23 -- wiki/aerospace/standard/ARP4754.org | 36 --- wiki/aerospace/standard/DO-160.org | 108 ------- wiki/aerospace/v-model.org | 42 --- 9 files changed, 609 deletions(-) delete mode 100644 wiki/aerospace/communication-protocols/ARINC-429.org delete mode 100644 wiki/aerospace/communication-protocols/CAN-bus.html delete mode 100644 wiki/aerospace/communication-protocols/CAN-bus.org delete mode 100644 wiki/aerospace/designing-aircraft.org delete mode 100644 wiki/aerospace/index.org delete mode 100644 wiki/aerospace/index.org.bkp delete mode 100644 wiki/aerospace/standard/ARP4754.org delete mode 100644 wiki/aerospace/standard/DO-160.org delete mode 100644 wiki/aerospace/v-model.org (limited to 'wiki/aerospace') 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 @@ - - - - - - - -CAN bus - - - - - - - -
-

CAN bus -
-A robust vehicle bus to enable hostless microcontroller communication. -

-
-

Table of Contents

-
- -
-
- - -
-

-ARP4754 is a guidance issued by SAE. -

- -
- - - - - -
-

2 Main topics

-
- - - --- -- -- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -
§ThemeDescription
1Development 
2Safety 
3Requirements mgmt. 
4Validation 
5Verification 
6Configuration mgmt. 
7Process assurance 
8Certification 
-
-
-
-
-

Date: 2022-03-25 Fri 00:00

-

Author: Marius Peter

-

Created: 2022-03-25 Fri 17:49

-

Validate

-
- - 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]] -- cgit v1.2.3