Editing IDS of OK "Buran"

Jump to navigation Jump to search

Warning: You are not logged in. Your IP address will be publicly visible if you make any edits. If you log in or create an account, your edits will be attributed to your username, along with other benefits.

The edit can be undone. Please check the comparison below to verify that this is what you want to do, and then save the changes below to finish undoing the edit.

Latest revision Your text
Line 1: Line 1:
This is a rough translation of the article titled "Information display system of the spacecraft "[[Buran program|Buran]]" by Tiapchenko. <ref>[http://www.cosmoworld.ru/spaceencyclopedia/publications/soi_buran.pdf soi_buran.pdf]</ref>
+
This is a rough translation of the article titled "Information display system of the spacecraft "Buran"" by Tiapchenko. [http://www.cosmoworld.ru/spaceencyclopedia/publications/soi_buran.pdf]
  
 
==Introduction==
 
==Introduction==
Line 5: Line 5:
 
The technical level of PI depends on the technical level of electronic and computer technology (EWT), electrical engineering and methods of data exchange with spacecraft systems. In this aspect, the IDS does not differ from the REA of general-purpose control systems (CS), and therefore there are no limitations for microminiaturization of it - there are no limitations in weight and dimensions.  
 
The technical level of PI depends on the technical level of electronic and computer technology (EWT), electrical engineering and methods of data exchange with spacecraft systems. In this aspect, the IDS does not differ from the REA of general-purpose control systems (CS), and therefore there are no limitations for microminiaturization of it - there are no limitations in weight and dimensions.  
 
The external part of the EI is the front panel of the console or dashboard, on which CO and OU are installed. Miniaturization, as a method of reducing the mass and dimensions, adopted in the REA for wide use, is practically inapplicable in EI, since the size of the OU, for example, depends on the capabilities of the human motoric apparatus (sizes of fingers, hands, legs, etc.). The dimensions of the selected COs depend on the size of the information displayed on them. The size of symbols or inscriptions depends on their distance from human eyes, etc.
 
The external part of the EI is the front panel of the console or dashboard, on which CO and OU are installed. Miniaturization, as a method of reducing the mass and dimensions, adopted in the REA for wide use, is practically inapplicable in EI, since the size of the OU, for example, depends on the capabilities of the human motoric apparatus (sizes of fingers, hands, legs, etc.). The dimensions of the selected COs depend on the size of the information displayed on them. The size of symbols or inscriptions depends on their distance from human eyes, etc.
 
==Structure of the IDS==
 
==Work organization for the IDS==
 
==Design features of the IDS==
 
==Ergonomic features of the IDS==
 
==Main characteristics of the IDS==
 
==Development of the spacecraft IDS==
 
==Main results and conclusions==
 
==Literature==
 
 
<references/>
 
 
[[Category: Articles]]
 
[[Category: Stubs]]
 

Please note that all contributions to OrbiterWiki are considered to be released under the GNU Free Documentation License 1.2 (see OrbiterWiki:Copyrights for details). If you do not want your writing to be edited mercilessly and redistributed at will, then do not submit it here.
You are also promising us that you wrote this yourself, or copied it from a public domain or similar free resource. Do not submit copyrighted work without permission!

To protect the wiki against automated edit spam, we kindly ask you to solve the following hCaptcha:

Cancel Editing help (opens in new window)