Inertially stabilized mirror system

• US 5,805,325 A
• Filed: 02/06/1997
• Issued: 09/08/1998
• Est. Priority Date: 10/25/1996
• Status: Expired due to Fees

• Current Assignee: Lockheed Martin Corporation (Martin Marietta Corporation)
• Original Assignee: Lockheed Martin Space Operations Company (Martin Marietta Corporation)
• Inventors: Clune, Lavern Charles
• Primary Examiner(s): Phan, James
• Application Number:
  US08/795,681
• Time in Patent Office: 579 Days
• Field of Search: 359/196, 359/197, 359/198, 359/201-203, 359/220, 359/221, 359/223, 359/226, 359/554-556, 359/872-874, 359/876, 359/900
• US Class Current: 359/226.1
• CPC Class Codes: G01C 21/18 Stabilised platforms, e.g. by gyroscope
• CPC Class Codes: G02B 27/644 compensating for large deviations, e.g. maintaining a fixed line of sight while a vehicle on which the system is mounted changes course
• CPC Class Codes: G02B 5/04 Prisms
• CPC Class Codes: G02B 7/007 Pressure-resistant sight glasses
• CPC Class Codes: Y10S 359/90 Methods

Abstract

Stabilization of pointing and stabilization mirror systems is provided by using the inherent moment of inertia of the mirrors. Inertially stabilized mirror systems have mirror orientations and rotation axes such that the mirrors reflect incident radiation parallel to the rotation axes. One mirror is provided for each axis of stabilization. In order to maintain stabilization in space for incident radiation to the mirror, any prior mirrors are provided with rotation axes parallel to the stabilization axis.

Claims

1. A method of using the inherent moment-of-inertia of a mirror mounted on a rotation axis to maintain orientation of the mirror and stabilization of the line-of-sight observed by an optical instrument mounted on a platform that experiences angular and translational disturbances, said method comprising,

mounting a first mirror for rotation about a first axis of rotation,

orienting the first mirror so that the first mirror reflects the incident radiation parallel to the first axis of rotation,

locating the center-of-mass of the first mirror on the first axis of rotation to prevent introduction of torque on the first mirror due to translational accelerations, and

using the inherent moment-of-inertia of the first mirror to maintain the orientation of the first mirror so as to result in a stabilized line-of-sight as observed by the optical instrument.

2. The invention defined in claim 1 including,

mounting a second mirror for rotation about a second axis of rotation,

mounting the first mirror for rotation about an axis of rotation which extends in the same direction as said second axis of rotation,

orienting the second mirror so that the second mirror receives the radiation reflected from said first mirror and reflects the radiation parallel to the second axis of rotation and on the line-of-sight to the optical instrument,

locating the center-of-mass of the second mirror on the second axis of rotation to prevent introduction of torque on the second mirror due to translational accelerations, and

using the inherent moment-of-inertia of the second mirror to maintain the orientation of the second mirror to provide stabilization of the line-of-sight of the optical instrument during said periods of angular and translational disturbances.

3. The invention defined in claim 2 wherein the first and second mirrors are mechanically coupled so that the first and second mirrors rotate together about said second axis.

4. The invention defined in claim 2 including,

mounting a third mirror for rotation about a third axis of rotation,

mounting the second mirror for rotation about an axis of rotation which extends in the same direction as said third axis of rotation,

orienting the third mirror so that the third mirror receives the radiation reflected from the second mirror and reflects the radiation parallel to the third axis of rotation and on the light of sight to the optical instrument,

locating the center-of-mass of the third mirror on the third axis of rotation to prevent introduction of torque on the third mirror due to translational accelerations, and

using the inherent moment-of-inertia of the third mirror to maintain the orientation of the third mirror to provide stabilization of the line-of-sight of the optical instrument during said periods of angular and translational disturbances.

5. The invention defined in claim 4 wherein the third axis of rotation is substantially orthogonal to the second axis of rotation and wherein the second axis of rotation is substantially orthogonal to the first axis of rotation.

6. The invention defined in claim 4 wherein the second and third mirrors are mechanically coupled so that the second and third mirrors rotate together about said third axis.

7. The invention defined in claim 4 wherein said using of the inherent moment of inertia of each of the mirrors about mirror rotation axes with said locating of the center-of-mass on the rotation axes provide said stabilization of the line-of-sight without the need to use active mirror controls or a gimbal mounting of the optical instrument.

8. The invention defined in claim 4 wherein said using the inherent moment of inertia of each of the mirrors about rotation axes with said locating of the center-of-mass on the rotation axes decouple the mirrors from the angular and translational disturbances experienced by said platform so that the mirrors stay still during such angular and translational disturbances.

9. Apparatus for using the inherent moment-of-inertia of a mirror mounted on a rotation axis to maintain orientation of the mirror and stabilization of the line-of-sight observed by an optical instrument mounted on a platform that experiences angular and translational disturbances, said apparatus comprising,

a first mirror mounted for rotation about a first axis of rotation,

said mirror being oriented so that the first mirror reflects the incident radiation parallel to the first axis of rotation,

said mirror having its center-of-mass located on the first axis of rotation to prevent introduction of torque on the first mirror due to translational accelerations, and

wherein the inherent moment-of-inertia of the first mirror maintains the orientation of the first mirror so as to result in a stabilized line-of-sight as observed by the optical instrument.

10. The invention defined in claim 9 including,

a second mirror mounted for rotation about a second axis of rotation,

said first mirror being also mounted for rotation about an axis of rotation which extends in the same direction as said second axis of rotation,

the second mirror being oriented so that the second mirror receives the radiation reflected from said first mirror and reflects the radiation parallel to the second axis of rotation and on the line-of-sight to the optical instrument,

said second mirror having its center-of-mass located on the second axis of rotation to prevent introduction of torque on the second mirror due to translational accelerations, and

wherein the inherent moment-of-inertia of the second mirror maintains the orientation of the second mirror to provide stabilization of the line-of-sight of the optical instrument during said periods of angular and translational disturbances.

11. The invention defined in claim 10 wherein the first and second mirrors are mechanically coupled to the first and second mirrors rotate together about said second axis.

12. The invention defined in claim 10 including,

a third mirror mounted for rotation about a third axis of rotation,

said second mirror being mounted for rotation about an axis of rotation which extends in the same direction as said third axis of rotation,

said third mirror being oriented so that the third mirror receives the radiation reflected from the second mirror and reflects the radiation parallel to the third axis of rotation and on the light of sight to the optical instrument,

said third mirror having its center-of-mass located on the third axis of rotation to prevent introduction of torque on the third mirror due to translational accelerations, and

wherein the inherent moment-of-inertia of the third mirror maintains the orientation of the third mirror to provide stabilization of the line-of-sight of the optical instrument during said periods of angular and translational disturbances.

13. The invention defined in claim 12 wherein the third axis of rotation is substantially orthogonal to the second axis of rotation and wherein the second axis of rotation is orthogonal to the first axis of rotation.

14. The invention defined in claim 12 wherein the second and third mirrors are mechanically coupled so that the second and third mirrors rotate together about said second axis.

15. The invention defined in claim 12 wherein said using of the inherent moment of inertia of each of the mirrors about mirror rotation axes with said locating of the center-of-mass on the rotation axes provide said stabilization of the line-of-sight without the need to use active mirror controls or a gimbal mounting of the optical instrument.

16. The invention defined in claim 12 wherein said using the inherent moment of inertia of each of the mirrors about rotation axes with said locating of the center-of mass on the rotation axes decouple the mirrors from the angular and translational disturbances experienced by said platform so that the mirrors stay still during such angular and translational disturbances.