Stabilization system for soft-mounted platform

• US 4,498,038 A
• Filed: 02/15/1983
• Issued: 02/05/1985
• Est. Priority Date: 02/15/1983
• Status: Expired due to Term

• Current Assignee: Richard M. Malueg
• Original Assignee: Richard M. Malueg
• Inventors: Malueg, Richard M.
• Primary Examiner(s): Dobeck, B.
• Application Number:
  US06/466,377
• Time in Patent Office: 721 Days
• Field of Search: 318/648, 318/649, 318/653, 354/74, 74/5.2, 248/550
• US Class Current: 318/648
• CPC Class Codes: B64D 47/08 Arrangements of cameras
• CPC Class Codes: F16F 15/03 using magnetic or electromagnetic means F16F9/53, F16F15/005 take precedence
• CPC Class Codes: G05D 3/1445 with a plurality of loops

Abstract

A stabilizing system for isolating a load device from vibrations of a supporting structure includes a pivotal member and a spring isolator connecting the load device to the supporting structure. Servo controlled actuators are connected across the pivotal member to rotate and torque the load relative to the isolator to compensate for angular displacement of the supporting structure and isolator relative to the load device. An inertial sensor secured to the load device provides a reference for the servo control.

Claims

1. Apparatus for stabilizing the motion of an inertial load relative to a supporting member, comprising:

an intermediate frame member, compliant isolation means connecting the intermediate frame member to the supporting member for providing limited translational motion of the intermediate member relative to the supporting member, pivot means connecting the load to the intermediate frame member, the pivot means allowing rotation of the load relative to the intermediate frame member about at least two mutual perpendicular axes of revolution, actuator means connected to the load and to the intermediate frame member for rotating the load relative to the intermediate frame member about each of said axes of revolution, and means for controlling said actuator means to adjust the angular position of the load relative to the intermediate frame about both said two axes of revolution.

2. Apparatus of claim 1 wherein said actuator means includes a two-axis linear actuator.

3. Apparatus of claim 2 wherein the linear actuator has a stator member forming a magnetic field extending across an air gap, and has an armature member movable linearly through the air gap in any direction substantially perpendicular to the direction of the magnetic field.

4. Apparatus of claim 3 wherein the stator and armature are rigidly anchored respectively to the load and the intermediate frame member.

5. Apparatus of claim 3 wherein the stator and armature are rigidly anchored respectively to the intermediate frame member and the load.

6. Apparatus of claim 1 wherein said actuator means includes first and second two-axis linear actuators.

7. Apparatus of claim 6 wherein the first and second two-axis linear actuators each have a stator member and an armature member movable linearly relative to the stator member in any direction extending substantially perpendicular to the direction of the magnetic field.

8. Apparatus for stabilizing a load against rotational motion about two or more mutually perpendicular axes and to isolate the load from translational vibrational motion relative to a support, said apparatus comprising:

pivot means having two relatively moving sections, the first section pivoting relative to the second section about at least two mutually perpendicular axes passing through the pivot point of said pivot means, compliant isolation means connecting the first section of the pivot means to the support, the isolation means providing limited translational movement of the pivot means relative to the support, the second section of the pivot means being rigidly connected to the load, actuator means having a drive member rigidly connected to one of the two sections of the pivot means and a drive member rigidly connected to the other of the two sections for rotating the two sections of the pivot means relative to each other about each of said mutually perpendicular axis, inertial sensor means connected to the load, and servo means responsive to the sensor means for driving the actuator means to adjust the relative angular position of the two sections about both of said axes and to correct for rotational movement of the first section of the pivot means by the support.

9. Apparatus of claim 8 wherein the pivot means comprises a gimbal system supporting the load from the isolator.

10. Apparatus of claim 8 wherein the pivot means provides relative rotation of the two sections about three mutually perpendicular axes.

11. Apparatus of claim 8 wherein the actuator means comprises a two-axis magnetic linear actuator.

12. Apparatus of claim 11 wherein the linear actuator means includes a magnetic field means for producing a magnetic field across a narrow gap, and moving coil means positioned in the gap, the field means being rigidly connected to one of said moving sections and the moving coil means being rigidly connected to the other of said moving sections.

13. Apparatus of claim 12 wherein the moving coil means includes two sets of coils arranged with the coils conducting current through the gap along mutually perpendicular paths.