Control of rotating mirrors

• US 4,626,063 A
• Filed: 12/12/1984
• Issued: 12/02/1986
• Est. Priority Date: 04/15/1983
• Status: Expired due to Fees

• Current Assignee: CARR BOYD Minerals Limited A Company Incorporated of Western Australa, Commonwealth Scientific & Industrial Research Organisation (Commonwealth Of Australia As Represented By Department Of Industry, Innovation, Climate Change, Science, Research And Tertiary Education)
• Original Assignee: CARR BOYD Minerals Limited A Company Incorporated of Western Australa, Commonwealth Scientific & Industrial Research Organisation (Commonwealth Of Australia As Represented By Department Of Industry, Innovation, Climate Change, Science, Research And Tertiary Education)
• Inventors: Honey, Frank R.
• Primary Examiner(s): Henry, Jon W.
• Application Number:
  US06/686,265
• Time in Patent Office: 720 Days
• Field of Search: 350/6.9, 350/6.5, 350/500, 350/632, 350/636, 350/486, 350/DIG. 3, 354/95, 250/235, 250/236
• US Class Current: 359/200.1
• CPC Class Codes: G01C 11/025 by scanning the object
• 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

Abstract

When producing images of the earth using rotating planar mirrors mounted in an aircraft, errors are introduced by roll, pitch and yaw of the aircraft. These errors are overcome in one of two ways. In the first way, the scanning planar mirror (30) is mounted on a shaft (54), the axis of which can be moved through small angles during the rotation of the shaft. This movement of the shaft is achieved by supporting the shaft (54) so that the end which does not carry the mirror is located within a cylindrical hollow region (60) at the end of an outer shaft (50). The two shafts rotate together. A pair of permanent magnets (51,52), each mounted axially in a respective shaft, have opposite poles adjacent to each other. The attraction of the magnets is perturbed by a transverse magnetic field established by an electromagnet (57,58,59) mounted outside the outer shaft (50). The current in the winding of the electromagnet depends upon the value of signals which are proportional to pitch and yaw of the aircraft. Those signals are derived from a gyroscope system (70). The second mechanism for overcoming errors involves mounting the scanning, planar mirror (12) in a cylinder (10) which is part of an inertial system that, in turn, is mounted on gimbals. Radiation received by the mirror is reflected by a system of mirrors which is similar to a Cassegrain telescope. The radiation is finally reflected by an elliptical mirror (18) to radiation monitoring equipment (21). In each case, signals indicative of the roll of the aircraft are used to control the time at which samples of the incoming radiation are first monitored.

Claims

1. A rotating mirror arrangement for use in airborne scanning comprising:

a. A first shaft of circular cross section, adapted to rotate about its axis, said shaft being hollow at one end thereof to provide a cylindrical region of circular cross section with said shaft;

b. a second shaft which is longer than the cylindrical region of the first shaft, said second shaft being supported within the cyindrical region of the first shaft by pivot means at or near the open end of said cylindrical region, said second shaft being pivotable about the axis of said pivot means, said axis being orthogonal to and passing through the axis of said first shaft, said second shaft being a loose fit in said cylindrical region;

c. a planar mirror mounted on the end of said second shaft which is outside said cylindrical region, the plane of said mirror being at 45°

relative to the axis of said second shaft;

d. a first elongate permanent magnet mounted within said first shaft along the axis thereof, a pole of said first permanent magnet being adjacent to the closed end of said hollow cylindrical region;

e. a second elongate permanent magnet mounted within said second shaft along the axis thereof, a pole of said second permanent magnet being adjacent to the end of said second shaft which is remote from said planar mirror so that said second permanent magnet is attracted by said first permanent magnet to bias the second shaft to a central position within the cylindrical region; and

f. electromagnet means fixedly positioned external to said first shaft to generate a magnetic field in the region of said pole of said second permanent magnet.

2. A rotating mirror arrangement as defined in claim 1 in which said electromagnet means is a monopole electromagnet.

3. A rotating mirror arrangement as defined in claim 1 in which said electromagnet means is a dipole electromagnet.

5. A rotating mirror arrangement as defined in claim 1 including means to balance said mirror and said second shaft both statically and dynamically.

6. A rotating mirror arrangement as defined in claim 5 in which said means to balance said mirror comprises a ring which is mounted with the plane of the ring orthogonal to the plane of said mirror, said ring being adapted to have small weights mounted thereon.

7. A rotating mirror arrangement as defined in claim 3 including balancing means to balance said mirror, said balancing means comprising a ring which is mounted with the plane of the ring orthogonal to the plane of said mirror, said ring being adapted to have small weights mounted thereon.

9. A rotating mirror arrangement as defined in claim 1, including:

a. a gyroscope system adapted to be mounted in an aircraft, said gyroscope system producing signals which are indicative of aircraft roll, pitch and yaw;

b. means responsive to the pitch and yaw signals generated by said gyroscope system to control the current through windings of said electromagnet means; and

c. means responsive to the roll signal generated by said gyroscope system to control the onset of sampling of radiation reflected by said mirror.

10. A rotating mirror arrangement as defined in claim 9, wherein said means responsive to the roll signal comprises a microprocessor and said means responsive to the pitch and roll signals comprises a first amplifier adapted to receive the pitch signal and a second amplifier adapted to receive the yaw signal, said amplifiers being connected to respective current sources for the windings of said electromagnet means.

13. A rotating mirror arrangement as defined in claim 10 wherein said electromagnet means is a dipole electromagnet.

4. A rotating mirror arrangement for use in airborne scanning comprising:

a. A first shaft of circular cross section adapted to rotate about its axis, said shaft being hollow at one end thereof to provide a cylindrical region of circular cross section within said shaft;

b. a second shaft which is longer than the cylindrical region of the first shaft, said second shaft being supported within the cylindrical region of the first shaft by a ball joint arrangement at or near the open end of said cylindrical region, said second shaft being pivotable about the axis of said ball joint arrangement, said axis being orthogonal to and passing through the axis of said first shaft, said second shaft being a loose fit in said cylindrical region;

c. a planar mirror mounted on the end of said second shaft which is outside said cylindrical region, the plane of said mirror being at 45°

relative to the axis of said second shaft;

d. a first elongate permanent magnet mounted within said first shaft along the axis thereof, a pole of said first permanent magnet being adjacent to the closed end of said hollow cylindrical region;

e. a second elongate permanent magnet mounted within said second shaft along the axis thereof, a pole of said second permanent magnet being adjacent to the end of said second shaft which is remote from said planar mirror, so that said second permanent magnet is attracted by said first permanent magnet, to bias the second shaft to a central position within the cylindrical region; and

f. a quadrapole electromagnet fixedly positioned external to said first shaft, to generate a magnetic field which controls the position of said second permanent magnet relative to said first permanent magnet.

8. A rotating mirror arrangement as defined in claim 4, including balancing means to balance said mirror, said balancing means comprising a ring which is mounted with the plane of the ring orthogonal to the plane of said mirror, said ring being adapted to have small weights mounted thereon.

11. A rotating mirror arrangement as defined in claim 4 including:

a. a gyroscope system adapted to be mounted in an aircraft, said gyroscope system producing signals which are indicative of aircraft roll, pitch and yaw;

b. means responsive to the pitch and yaw signals generated by said gyroscope system to control the current through windings of said electromagnet; and

c. means responsive to the roll signal generated by said gyroscope system to control the onset of sampling of radiation reflected by said mirror.

12. A rotating mirror arrangement as defined in claim 11 wherein said means responsive to the roll signal comprises a microprocessor and said means responsive to the pitch and roll signals comprises a first amplifier adapted to receive the pitch signal and a second amplifier adapted to receive the yaw signal, said amplifiers being connected to respective current sources for the windings of said electromagnet.