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US3601338A Expired / Lapsed US ⏱️ 0.0 years remaining

Apparatus for controlling the attitude of a satellite

Assignee: Toshiba Corp
•
Filing: 1968-11-14
•
Granted: 1971-08-24
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Expires: 1988-11-14
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Abstract

Abstract An attitude-control apparatus for a satellite includes a main rod extending from the satellite body and having a weight at the outermost end thereof, and a rotatable damping rod supported on the satellite body. Damping control is effected by detecting the deflection of the satellite body from the standard direction in an inertial space thereby to vibrate the damping rod in the direction opposite to that of the deflection.

Inventors

  • 👤 Masamichi Shigehara

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-30 16:25
CPC Classifications
B; B64; B64G; B64G1/00; B64G1/22; B64G1/24; B64G1/38; B64G1/244; B64G1/32; B64G1/34

Claims Analysis

Total Claims: 5
Claim 1
Independent Claim 186 words
An apparatus for controlling the attitude of a satellite comprising: a satellite body (11); a main rod (12) fixedly coupled to and extending from the satellite body (11) and provided with a weight at the outermost end thereof to control the attitude of the satellite body using the gravity gradient torque; a damping rod (13) extending from the main rod (12) and movably connected thereto; an actuating means (41) coupled to said damping rod (13) for moving said damping rod (13) relative to said main rod (12); a damper (14) interposed between the main rod (12) and the damping rod (13); an attitude-detector means (34) for detecting the deflection angles of said satellite body (11) and of the main rod (12) from the standard direction in the inertial space independent of the position of said damping rod (13); and control means (36, 37, 38, 39) responsive to the output of said attitude-detector means (34) for driving said actuating means (41) to control said damping rod (13) to cause said damping rod (13) to rotate in a direction opposite to that which said satellite body (11) vibrates.
Claim 2
Independent Claim 186 words
An apparatus for controlling the attitude of a satellite comprising: a satellite body (11); a main rod (12) fixedly coupled to and extending from the satellite body (11) and provided with a weight at the outermost end thereof to control the attitude of the satellite body using the gravity gradient torque; a damping rod (13) extending from the main rod (12) and movably connected thereto; an actuating means (41) coupled to said damping rod (13) for moving said damping rod (13) relative to said main rod (12); a damper (14) interposed between the main rod (12) and the damping rod (13); an attitude-detector means (34) for detecting the deflection angles of said satellite body (11) and of the main rod (12) from the standard direction in the inertial space independent of the position of said damping rod (13); and control means (36, 37, 38, 39) responsive to the output of said attitude-detector means (34) for driving said actuating means (41) to control said damping rod (13) to cause said damping rod (13) to rotate in a direction opposite to that which said satellite body (11) vibrates.
Claim 3
Dependent Claim 67 words
Apparatus according to claim 1 wherein said control means comprises: means (36) for changing the sign and gain of electrical outputs from said attitude detector (34) which correspond to the angles of deflection; and a servocontrol means (37, 38, 39) for driving said actuating means (41) so as to rotate said damping rod (13) in said direction opposite to that in which said satellite body (11) vibrates.
Claim 4
Dependent Claim 14 words
Apparatus according to claim 1 wherein said attitude detector (34) includes a horizon sensor.
Claim 5
Dependent Claim 14 words
Apparatus according to claim 1 wherein said attitude detector (34) includes a sun sensor.

References Cited (Backward Citations)

US3168263A Cited
US3243143A Cited
US3268183A Cited
US3282532A Cited
US3302905A Cited
US3358945A Cited
US3519222A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1974-08-23 1975-02-22 1975-08-24 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1978-08-23 1979-02-22 1979-08-24 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1982-08-23 1983-02-22 1983-08-24 $7700.00 Window Closed / Lapsed

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