SE9602403L - Satellite simulation device - Google Patents

Satellite simulation device

Info

Publication number
SE9602403L
SE9602403L SE9602403A SE9602403A SE9602403L SE 9602403 L SE9602403 L SE 9602403L SE 9602403 A SE9602403 A SE 9602403A SE 9602403 A SE9602403 A SE 9602403A SE 9602403 L SE9602403 L SE 9602403L
Authority
SE
Sweden
Prior art keywords
satellite
around
arm
support component
axis
Prior art date
Application number
SE9602403A
Other languages
Unknown language ( )
Swedish (sv)
Other versions
SE9602403D0 (en
SE504926C2 (en
Inventor
Boerje Rautio
Birger Eriksson
Original Assignee
Micsat Ab
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Micsat Ab filed Critical Micsat Ab
Priority to SE9602403A priority Critical patent/SE504926C2/en
Publication of SE9602403D0 publication Critical patent/SE9602403D0/en
Publication of SE9602403L publication Critical patent/SE9602403L/en
Publication of SE504926C2 publication Critical patent/SE504926C2/en

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

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).
SE9602403A 1996-06-18 1996-06-18 Path simulator for satellites SE504926C2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SE9602403A SE504926C2 (en) 1996-06-18 1996-06-18 Path simulator for satellites

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SE9602403A SE504926C2 (en) 1996-06-18 1996-06-18 Path simulator for satellites

Publications (3)

Publication Number Publication Date
SE9602403D0 SE9602403D0 (en) 1996-06-18
SE9602403L true SE9602403L (en) 1997-05-26
SE504926C2 SE504926C2 (en) 1997-05-26

Family

ID=20403055

Family Applications (1)

Application Number Title Priority Date Filing Date
SE9602403A SE504926C2 (en) 1996-06-18 1996-06-18 Path simulator for satellites

Country Status (1)

Country Link
SE (1) SE504926C2 (en)

Also Published As

Publication number Publication date
SE9602403D0 (en) 1996-06-18
SE504926C2 (en) 1997-05-26

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