U.S. patents available from 1976 to present.
U.S. patent applications available from 2005 to present.

Solar array stepping to minimize array excitation

Patent 4843294 Issued on June 27, 1989. Estimated Expiration Date: Icon_subject December 1, 2007. Estimated Expiration Date is calculated based on simple USPTO term provisions. It does not account for terminal disclaimers, term adjustments, failure to pay maintenance fees, or other factors which might affect the term of a patent.

Patent References

3188546

Method of positioning a moving part and a printer operating in accordance with said method
Patent #: 4258622
Issued on: 03/31/1981
Inventor: Estrabaud ,   et al.

Dual turntable record player with torque cancellation
Patent #: 4425638
Issued on: 01/10/1984
Inventor: Suzuki ,   et al.

Record player with vibration cancellation mechanism
Patent #: 4475185
Issued on: 10/02/1984
Inventor: Fujio ,   et al.

Torque loop control system and method
Patent #: 4481453
Issued on: 11/06/1984
Inventor: Welburn

Active damping of satellite nutation Patent #: 4732354
Issued on: 03/22/1988
Inventor: Lievre

Inventors

Assignee

Application

No. 07/127344 filed on 12/01/1987

US Classes:

318/696, OPEN-LOOP STEPPING MOTOR CONTROL SYSTEMS244/170, By nutation damper318/460, Sound, supersonic vibration or mechanical vibration318/685, "Step-by-step" motors in closed-loop servos369/265With auxiliary turntable

Examiners

Primary: Shoop, William M. Jr.
Assistant: Bergmann, Saul M.

Attorney, Agent or Firm

International Classes

G05D 19/02 (20060101)
G05D 1/08 (20060101)
G05D 19/00 (20060101)
B64G 1/42 (20060101)
B64G 1/44 (20060101)

Abstract

Mechanical oscillations of a mechanism containing a stepper motor, such as a solar-array powered spacecraft, are reduced and minimized by the execution of step movements in pairs of steps, the period between steps being equal to one-half of the period of torsional oscillation of the mechanism. Each pair of steps is repeated at needed intervals to maintain desired continuous movement of the portion of elements to be moved, such as the solar array of a spacecraft. In order to account for uncertainty as well as slow change in the period of torsional oscillation, a command unit may be provided for varying the interval between steps in a pair.

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