Orion guidance, navigation, and control system
E1000721
The Orion guidance, navigation, and control system is the spacecraft’s integrated suite of sensors, computers, and software that determines its position and orientation and precisely controls its trajectory and attitude during missions beyond low Earth orbit.
All labels observed (1)
| Label | Occurrences |
|---|---|
| Orion guidance, navigation, and control system canonical | 1 |
How this entity was disambiguated
This entity first appeared as the object of triple T12738316 — 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: Orion guidance, navigation, and control system Context triple: [Exploration Flight Test 1, testedSystem, Orion guidance, navigation, and 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.
Voyager 2 attitude control system
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.
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C.
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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D.
Orbital Maneuvering System
The Orbital Maneuvering System was the Space Shuttle’s pair of rear-mounted rocket engines used for orbital insertion, adjustment, and deorbit burns.
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E.
Orion spacecraft
The Orion spacecraft is NASA’s next-generation crewed space vehicle designed to carry astronauts beyond low Earth orbit on deep-space missions, including journeys to the Moon and eventually Mars.
- F. None of above. chosen
- G. Unsure - the case is ambiguous/there is not enough information to decide.
Target entity: Orion guidance, navigation, and control system Target entity description: The Orion guidance, navigation, and control system is the spacecraft’s integrated suite of sensors, computers, and software that determines its position and orientation and precisely controls its trajectory and attitude during missions beyond low Earth orbit.
-
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.
Voyager 2 attitude control system
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.
-
C.
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.
-
D.
Orbital Maneuvering System
The Orbital Maneuvering System was the Space Shuttle’s pair of rear-mounted rocket engines used for orbital insertion, adjustment, and deorbit burns.
-
E.
Orion spacecraft
The Orion spacecraft is NASA’s next-generation crewed space vehicle designed to carry astronauts beyond low Earth orbit on deep-space missions, including journeys to the Moon and eventually Mars.
- F. None of above. chosen
Statements (49)
| Predicate | Object |
|---|---|
| instanceOf |
avionics subsystem
ⓘ
spacecraft guidance, navigation, and control system ⓘ |
| controls |
Orion main propulsion system pointing
ⓘ
Orion reaction control system NERFINISHED ⓘ spacecraft attitude during burns ⓘ spacecraft attitude during coast phases ⓘ |
| designedFor |
deep space environment
ⓘ
fault tolerance ⓘ high-reliability operation ⓘ |
| developedFor |
NASA Artemis program
NERFINISHED
ⓘ
missions beyond low Earth orbit ⓘ |
| developer | NASA NERFINISHED ⓘ |
| hasComponent |
GN&C software
ⓘ
actuator control electronics ⓘ flight computers ⓘ navigation sensors ⓘ |
| hasFunction |
control spacecraft attitude
ⓘ
control spacecraft trajectory ⓘ determine spacecraft orientation ⓘ determine spacecraft position ⓘ execute control laws ⓘ perform guidance computations ⓘ perform navigation filtering ⓘ |
| integrates |
GPS receivers
ⓘ
inertial measurement units ⓘ main engine gimbals ⓘ optical navigation sensors ⓘ reaction control system actuators ⓘ star trackers ⓘ |
| operatesIn |
cislunar space
ⓘ
low Earth orbit ⓘ |
| partOf |
NASA Orion crew vehicle
NERFINISHED
ⓘ
Orion spacecraft NERFINISHED ⓘ |
| performs |
attitude control
ⓘ
autonomous navigation ⓘ closed-loop guidance ⓘ onboard state estimation ⓘ |
| supports |
crewed missions
ⓘ
uncrewed test flights ⓘ |
| supportsMissionPhase |
Earth orbit operations
ⓘ
cislunar navigation ⓘ entry, descent, and splashdown ⓘ launch ⓘ lunar return trajectory ⓘ trans-lunar injection ⓘ |
| usedOnMission | Artemis I NERFINISHED ⓘ |
| uses |
computers
ⓘ
sensors ⓘ software ⓘ |
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: Orion guidance, navigation, and control system Description of subject: The Orion guidance, navigation, and control system is the spacecraft’s integrated suite of sensors, computers, and software that determines its position and orientation and precisely controls its trajectory and attitude during missions beyond low Earth orbit.
Referenced by (1)
Full triples — surface form annotated when it differs from this entity's canonical label.