SE9602403D0 - Satellite simulation device - Google Patents
Satellite simulation deviceInfo
- Publication number
- SE9602403D0 SE9602403D0 SE9602403A SE9602403A SE9602403D0 SE 9602403 D0 SE9602403 D0 SE 9602403D0 SE 9602403 A SE9602403 A SE 9602403A SE 9602403 A SE9602403 A SE 9602403A SE 9602403 D0 SE9602403 D0 SE 9602403D0
- Authority
- SE
- Sweden
- Prior art keywords
- satellite
- around
- arm
- support component
- axis
- Prior art date
Links
Classifications
-
- G—PHYSICS
- G09—EDUCATION; CRYPTOGRAPHY; DISPLAY; ADVERTISING; SEALS
- G09B—EDUCATIONAL OR DEMONSTRATION APPLIANCES; APPLIANCES FOR TEACHING, OR COMMUNICATING WITH, THE BLIND, DEAF OR MUTE; MODELS; PLANETARIA; GLOBES; MAPS; DIAGRAMS
- G09B9/00—Simulators for teaching or training purposes
- G09B9/02—Simulators for teaching or training purposes for teaching control of vehicles or other craft
- G09B9/52—Simulators for teaching or training purposes for teaching control of vehicles or other craft for teaching control of an outer space vehicle
Landscapes
- Engineering & Computer Science (AREA)
- Theoretical Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Business, Economics & Management (AREA)
- Physics & Mathematics (AREA)
- Educational Administration (AREA)
- Educational Technology (AREA)
- General Physics & Mathematics (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
- Toys (AREA)
Abstract
The device incorporates a satellite (1) which, borne by support component (2), is arranged to execute a circulating movement in a path around an artificial celestial body (3), preferably in the form of an earth globe. Manoeuvring units are arranged on the support component for attitude control of the satellite during its circular movement around the artificial celestial body. The manoeuvring units can be activated for adjustment by a guide and control unit. The artificial celestial body can be placed on a base and the support component comprises an arm (5) rotatably fixed to the body. The arm can pivot around an axis (6) extending vertically through the body. At the end of the arm a carriage (7) is supported by the base and at least one wheel drives the carriage and thereby the arm. The manoeuvring units for attitude control of the satellite comprise one unit for pivoting the satellite around an axis parallel to the movement direction (23) and one unit for pivoting the satellite around an axis at right-angles to the movement direction (25).
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SE9602403A SE9602403L (en) | 1996-06-18 | 1996-06-18 | Satellite simulation device |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SE9602403A SE9602403L (en) | 1996-06-18 | 1996-06-18 | Satellite simulation device |
Publications (3)
Publication Number | Publication Date |
---|---|
SE9602403D0 true SE9602403D0 (en) | 1996-06-18 |
SE504926C2 SE504926C2 (en) | 1997-05-26 |
SE9602403L SE9602403L (en) | 1997-05-26 |
Family
ID=20403055
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SE9602403A SE9602403L (en) | 1996-06-18 | 1996-06-18 | Satellite simulation device |
Country Status (1)
Country | Link |
---|---|
SE (1) | SE9602403L (en) |
-
1996
- 1996-06-18 SE SE9602403A patent/SE9602403L/en not_active IP Right Cessation
Also Published As
Publication number | Publication date |
---|---|
SE504926C2 (en) | 1997-05-26 |
SE9602403L (en) | 1997-05-26 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
NUG | Patent has lapsed |
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