Difference between revisions of "Sirius-7K IDS"
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;КЛП | ;КЛП | ||
:Logic switching unit | :Logic switching unit | ||
+ | ;КПЛ | ||
+ | :Command receiver | ||
;ПВУ | ;ПВУ | ||
:Program timing device | :Program timing device |
Revision as of 22:26, 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 |
КСУ 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
- БДУС
- Rate gyroscope assembly system
- БКИД
- Ion flow sensor control system
- ДО
- 10N attitude control vernier thrusters.
- ДПО
- 100N attitude control and maneuvering thrusters.
- ЗСП
- Reserve parachute
- ИД
- Ion flow sensor
- ИКПВ
- Инфракрасный Построитель Вертикали, Infrared vertical sensor
- КСУ
- Command/Signal Unit
- КЛП
- Logic switching unit
- КПЛ
- Command receiver
- ПВУ
- Program timing device
- ПК
- Control panel
- СД
- Sun sensor
- СКД
- Main engine
- СОУД
- Attitude and motion control system
- ССВП
- Docking and internal transfer system