Difference between revisions of "Sirius-7K IDS"

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Line 175: Line 175:
  
 
==Combined Electronic Indicator (CEI)==
 
==Combined Electronic Indicator (CEI)==
 +
 +
==Electroluminescent Signal Indicator==
 +
 +
{|
 +
|style="background-color:red;color=white;"|Radiation in DM
 +
|style="background-color:red;color=white;"|Undocking
 +
|style="background-color:red;color=white;"|Low pressure in DM
 +
|style="background-color:red;color=white;"|Air composition
 +
|-
 +
|style="background-color:red;color=white;"|ССВП Mode
 +
|style="background-color:red;color=white;"|Back-up Parachute
 +
|style="background-color:red;color=white;"|Launcher Malfunction
 +
|style="background-color:red;color=white;"|Temperature sensor triggered
 +
|-
 +
|style="background-color:red;color=white;"|
 +
|style="background-color:red;color=white;"|Back-up battery
 +
|style="background-color:red;color=white;"|
 +
|style="background-color:red;color=white;"|Depressurization of CTP
 +
|-
 +
|style="background-color:yellow;"|Ballistic Descent
 +
|style="background-color:yellow;"|Low Voltage
 +
|style="background-color:yellow;"|Guidance on roll
 +
|style="background-color:yellow;"|Hatch OM-DM open
 +
|-
 +
|style="background-color:yellow;"|Panel lock removed
 +
|style="background-color:yellow;"|Fasten seat belts
 +
|style="background-color:yellow;"|Input axis
 +
|style="background-color:yellow;"|Landing
 +
|-
 +
|style="background-color:yellow;"|Uplink
 +
|style="background-color:yellow;"|Transmitter ДРК on
 +
|style="background-color:yellow;"|Gyroscopes uncaged
 +
|style="background-color:yellow;"|
 +
|-
 +
|style="background-color:yellow;"|Radio session
 +
|style="background-color:yellow;"|
 +
|style="background-color:yellow;"|ДПО nozzle
 +
|style="background-color:yellow;"|Attitude
 +
|-
 +
|style="background-color:yellow;"|ССВП Mode
 +
|style="background-color:yellow;"|
 +
|style="background-color:yellow;"|Capture
 +
|style="background-color:yellow;"|
 +
|-
 +
|style="background-color:yellow;"|Bad port docked
 +
|style="background-color:yellow;"|ДО nozzle
 +
|style="background-color:yellow;"|
 +
|style="background-color:yellow;"|СКДУ activated
 +
|}
  
 
==Acronyms==
 
==Acronyms==
Line 189: Line 238:
 
;СОУД
 
;СОУД
 
:Attitude and motion control system
 
:Attitude and motion control system
 +
;ССВП
 +
:Docking and internal transfer system
  
 
==References==
 
==References==
 
* [http://www.cosmoworld.ru/spaceencyclopedia/publications/soyuz7.pdf Системы отображения информации типа "Сириус" космических аппаратов "Союз-7К","Союз-А8","Союз-М",станций "ДОС-17К"]
 
* [http://www.cosmoworld.ru/spaceencyclopedia/publications/soyuz7.pdf Системы отображения информации типа "Сириус" космических аппаратов "Союз-7К","Союз-А8","Союз-М",станций "ДОС-17К"]
 
* [http://www.cosmoworld.ru/spaceencyclopedia/publications/analiz.pdf Анализ и синтез подсистем СОИ ПКА]
 
* [http://www.cosmoworld.ru/spaceencyclopedia/publications/analiz.pdf Анализ и синтез подсистем СОИ ПКА]

Revision as of 21:56, 9 October 2010

Command/Signal instrument (CSI)

CSI - a first type of an integrated control panel. It controls guidance systems and subsystems of spacecraft 7K-OK, signalizes executed commands, monitors the state of complex systems. In the IDS Sirius-7K are two CSIs: A left CSI and a right CSI.

Command/Signal matrix (English translation)

A Б B Г Д Е Ж И К Л М Н П Р С Т
Backup
Radio 		Radio D/L Landing ECLSS
DM 		ECLSS
OM, PM 		Airlock Docking Prepare
Reentry
Guidance 		Attitude
Control
System 		Navigation Program Propellant
Supply
System 		Back-up
System 		RTS, RKO
KM, SEP 		CEI
1 2 Prepare
UHF XMTR
I 		Modulation
HF and UHF 		АСП Light I Guide
from DM 		Prepare
RDZ 		Select
ДПО 		Cancel
Mode 		Manual
Control 		Cancel
program 		RCS
tanks 		Habitat
Systems 		RTS, RKO CEI
3 4 Prepare
UHF XMTR
II 		Back-up UHF
antenna 		Air supply
Valve 		Light II Dryer Supply
interface 		Retract
Probe (?) 		Select
ДО 		DU Orbit
maneuver 		ДО nozzle Propulsion
System 		Back-up
Antenna I 		Air
assembly
5 6 UHF RVR
Simplex 		Dynamic
OM 		XMTR mode
Voice / Recorder 		Transfer
light 		Reduce
Press. in
OM 		Manual docking Indicator
mode 		RO βс Approach "IE" Supply ДО Sealed
Enclosure
A / B 		Antenna II
7 8 UHF RCVR
Duplex 		Microphone Transmit ??????
Light Ctrl. 		PO Valve Egress
Hatch
open 		Lateral
offset
connection 		ИД разг.тор Pulsed RO γс Automated
deorbit 		Pressurize
ДО 		PTD
P gr 		Matrix I Off Fast pitch
9 10 Prepare
HF XMTR II 		Pyro-String I Gas analysis AC
OM 		Basic
press.
open 		TV Camera
A 		Pitch
forward 		IO αх Deorbit
by RO 		Supply
ДПО 		Television Matrix II Off Peroxide
ДПО
11 12 Prepare
HF XMTR I 		Pyro-String II Dehumidify Inner Pump Tank
press.
open 		TV Camera
B 		Pitch
backward 		Sun
tracking 		СКД
impulse 		Automatic
Maneuver 		Pressurize
ДПО 		Power СОУД VKIP off
13 14 Frequency
HF XMTR I 		Telegraph Pyro-String
ЗСП 		Dryer Outer Pump I TV Camera OM TV scale
Fluid/Manual 		Visor
attitude 		Manual
input 		Maneuver
with RO 		Engine Generator
setting 		Solar battery
off

Combined Electronic Indicator (CEI)

Electroluminescent Signal Indicator

Radiation in DM Undocking Low pressure in DM Air composition
ССВП Mode Back-up Parachute Launcher Malfunction Temperature sensor triggered
Back-up battery Depressurization of CTP
Ballistic Descent Low Voltage Guidance on roll Hatch OM-DM open
Panel lock removed Fasten seat belts Input axis Landing
Uplink Transmitter ДРК on Gyroscopes uncaged
Radio session ДПО nozzle Attitude
ССВП Mode Capture
Bad port docked ДО nozzle СКДУ activated

Acronyms

АСП
Automatic landing program
ДО
10N attitude control vernier thrusters.
ДПО
100N attitude control and maneuvering thrusters.
ЗСП
Reserve parachute
СКД
Main engine
СОУД
Attitude and motion control system
ССВП
Docking and internal transfer system

References

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