Attitude and Articulation Control Subsystem computer
E49821
The Attitude and Articulation Control Subsystem computer is the dedicated onboard system on Voyager 2 responsible for controlling the spacecraft’s orientation and the pointing of its instruments and antennas.
Observed surface forms (1)
| Surface form | Occurrences |
|---|---|
| Attitude and Articulation Control Subsystem | 2 |
Statements (46)
| Predicate | Object |
|---|---|
| instanceOf |
attitude control computer
ⓘ
spacecraft onboard computer ⓘ |
| associatedWith |
Voyager 2 articulation mechanisms
ⓘ
Voyager 2 attitude control system ⓘ |
| communicatesWith |
Voyager 2 attitude control system
ⓘ
surface form:
Voyager 2 Command Computer Subsystem
Voyager 2 ⓘ
surface form:
Voyager 2 Flight Data Subsystem
|
| controls |
articulation of antennas
ⓘ
articulation of instruments ⓘ pointing of antennas ⓘ pointing of instruments ⓘ spacecraft attitude ⓘ spacecraft orientation ⓘ thruster firings for attitude control ⓘ |
| designedBy | Jet Propulsion Laboratory ⓘ |
| ensures |
high-gain antenna Earth-pointing
ⓘ
proper pointing of science instruments ⓘ stable communication link with Earth ⓘ |
| hardwareGeneration | 1970s ⓘ |
| implements |
articulation control algorithms
ⓘ
attitude control algorithms ⓘ |
| launchDate | 1977-08-20 ⓘ |
| launchVehicle | Titan IIIE-Centaur ⓘ |
| location |
Voyager 2
ⓘ
surface form:
Voyager 2 spacecraft bus
|
| mission | Voyager program ⓘ |
| missionPhase |
interstellar mission
ⓘ
planetary flybys ⓘ |
| monitors |
Sun sensors
ⓘ
attitude sensors ⓘ gyroscopes ⓘ star trackers ⓘ |
| operator | NASA ⓘ |
| partOf | Voyager 2 ⓘ |
| powerSource | radioisotope thermoelectric generators ⓘ |
| primaryFunction |
control scan platform motion
ⓘ
execute attitude correction maneuvers ⓘ maintain correct spacecraft pointing ⓘ |
| role |
autonomous control of spacecraft pointing
ⓘ
execution of stored attitude sequences ⓘ |
| spacecraft | Voyager 2 ⓘ |
| spacecraftType | interplanetary probe ⓘ |
| status | operational for decades after launch ⓘ |
| subsystemOf |
Attitude and Articulation Control Subsystem computer
self-linksurface differs
ⓘ
surface form:
Attitude and Articulation Control Subsystem
|
| usedFor |
spin control during early mission phases
ⓘ
three-axis stabilization ⓘ |
| uses |
attitude reference data
ⓘ
reaction control thrusters ⓘ |
Referenced by (3)
Full triples — surface form annotated when it differs from this entity's canonical label.
this entity surface form:
Attitude and Articulation Control Subsystem
Attitude and Articulation Control Subsystem computer
→
subsystemOf
→
Attitude and Articulation Control Subsystem computer
self-linksurface differs
ⓘ
this entity surface form:
Attitude and Articulation Control Subsystem