Voyager 2 attitude control system
E242352
The Voyager 2 attitude control system is the spacecraft’s subsystem responsible for precisely orienting and stabilizing the probe in space so its instruments and communications antenna remain correctly pointed.
All labels observed (4)
How this entity was disambiguated
This entity first appeared as the object of triple T2189225 — resolving that mention is where its identity was fixed. The disambiguator weighed these candidate entities and picked the highlighted one (or “None”, minting a new entity). This is how homonymy is resolved: the same surface form can point to different entities.
Target entity: Voyager 2 attitude control system Context triple: [Attitude and Articulation Control Subsystem computer, associatedWith, Voyager 2 attitude control system]
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A.
Fine Guidance Sensor
The Fine Guidance Sensor is a high-precision pointing and stabilization instrument on the James Webb Space Telescope that locks onto guide stars to keep the observatory accurately aimed during observations.
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B.
Spacelab instrument pointing system
The Spacelab instrument pointing system was a precision guidance and control platform that allowed scientific instruments on Spacelab to be accurately aimed and stabilized for observations in space.
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C.
Spartan-Halley free-flyer
Spartan-Halley free-flyer was an autonomous, reusable NASA spacecraft designed to study Halley’s Comet by conducting short-duration, targeted observations while deployed from and later retrieved by the Space Shuttle.
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D.
Hubble Space Telescope Fine Guidance Sensors
The Hubble Space Telescope Fine Guidance Sensors are high-precision optical instruments that both keep Hubble accurately pointed at astronomical targets and serve as scientific tools for measuring stellar positions and distances.
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E.
Pioneer Venus project
The Pioneer Venus project was a NASA mission in the late 1970s that sent an orbiter and multiple probes to study Venus’s atmosphere, surface, and environment in unprecedented detail.
- F. None of above. chosen
- G. Unsure - the case is ambiguous/there is not enough information to decide.
Target entity: Voyager 2 attitude control system Target entity description: The Voyager 2 attitude control system is the spacecraft’s subsystem responsible for precisely orienting and stabilizing the probe in space so its instruments and communications antenna remain correctly pointed.
-
A.
Fine Guidance Sensor
The Fine Guidance Sensor is a high-precision pointing and stabilization instrument on the James Webb Space Telescope that locks onto guide stars to keep the observatory accurately aimed during observations.
-
B.
Spacelab instrument pointing system
The Spacelab instrument pointing system was a precision guidance and control platform that allowed scientific instruments on Spacelab to be accurately aimed and stabilized for observations in space.
-
C.
Spartan-Halley free-flyer
Spartan-Halley free-flyer was an autonomous, reusable NASA spacecraft designed to study Halley’s Comet by conducting short-duration, targeted observations while deployed from and later retrieved by the Space Shuttle.
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D.
Hubble Space Telescope Fine Guidance Sensors
The Hubble Space Telescope Fine Guidance Sensors are high-precision optical instruments that both keep Hubble accurately pointed at astronomical targets and serve as scientific tools for measuring stellar positions and distances.
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E.
Pioneer Venus project
The Pioneer Venus project was a NASA mission in the late 1970s that sent an orbiter and multiple probes to study Venus’s atmosphere, surface, and environment in unprecedented detail.
- F. None of above. chosen
Statements (45)
| Predicate | Object |
|---|---|
| instanceOf |
spacecraft attitude control system
ⓘ
subsystem of Voyager 2 ⓘ |
| commands |
attitude control thruster firings
ⓘ
reaction wheel speed changes ⓘ |
| controls | three-axis orientation of Voyager 2 ⓘ |
| coordinatesWith |
Voyager 2 power subsystem
ⓘ
Voyager 2 science instruments ⓘ Voyager 2 telecommunications subsystem ⓘ |
| criticalFor |
data return from Voyager 2
ⓘ
spacecraft survival in deep space ⓘ |
| designedBy | Voyager project engineering team ⓘ |
| designedFor |
deep-space operations
ⓘ
long-duration mission lifetime ⓘ |
| ensures |
high-gain antenna Earth-pointing accuracy
ⓘ
instrument boresight pointing accuracy ⓘ |
| environment |
interplanetary space
ⓘ
interstellar space ⓘ |
| epoch | 1970s spacecraft engineering ⓘ |
| implements |
attitude determination algorithms
ⓘ
closed-loop attitude control ⓘ safe-mode pointing strategies ⓘ |
| maintains | spin and tumble stability of Voyager 2 ⓘ |
| mission | Voyager 2 mission to outer planets and interstellar space ⓘ |
| monitors | spacecraft attitude sensors ⓘ |
| mustHandle |
aging hardware components
ⓘ
limited propellant resources ⓘ weak solar illumination at large heliocentric distances ⓘ |
| operatedBy |
Jet Propulsion Laboratory
ⓘ
surface form:
NASA Jet Propulsion Laboratory
|
| operatesOn | Voyager 2 spacecraft body orientation ⓘ |
| partOf |
Voyager 2
ⓘ
Voyager 2 attitude control system self-linksurface differs ⓘ
surface form:
Voyager 2 guidance, navigation, and control system
|
| primaryFunction |
maintain spacecraft attitude
ⓘ
point high-gain antenna toward Earth ⓘ point scientific instruments toward targets ⓘ stabilize spacecraft rotation ⓘ |
| supports |
imaging observations of planets and moons
ⓘ
in-situ measurements alignment ⓘ radio communications link with Earth ⓘ |
| uses |
gyroscopes
ⓘ
inertial reference units ⓘ onboard computer control algorithms ⓘ reaction wheels ⓘ star trackers ⓘ sun sensors ⓘ thrusters ⓘ |
How these facts were elicited
The pipeline generated the facts above by prompting gpt-5.1 with this entity's name + description and the instruction below.
You are a knowledge base construction expert. Given a subject entity and a description of it, return factual statements that you know for the subject as a JSON list of dictionaries(triples), where keys must be "subject", "predicate" and "object". The number of facts may be very high, between 25 to 50 or more, for very popular subjects. For less popular subjects, the number of facts can be very low, like 5 or 10. # Requirements - If you don't know the subject at all, return an empty list. - If the subject is not a named entity, return an empty list. - Include at least one triple where predicate is "instanceOf". - Do not get too wordy. - Separate several objects into multiple triples with one object.
Subject: Voyager 2 attitude control system Description of subject: The Voyager 2 attitude control system is the spacecraft’s subsystem responsible for precisely orienting and stabilizing the probe in space so its instruments and communications antenna remain correctly pointed.
Referenced by (4)
Full triples — surface form annotated when it differs from this entity's canonical label.