Viewing apparatus with a counterbalanced and articulated mirror

• US 5,815,302 A
• Filed: 10/11/1995
• Issued: 09/29/1998
• Est. Priority Date: 10/11/1995
• Status: Expired due to Term

• Current Assignee: OL Security LLC (Intellectual Ventures LLC)
• Original Assignee: Hughes Electronics Corporation (Rtx Corporation)
• Inventors: Mc Vey, Ray E., Wu, Yeong-Wei A., Anagnost, John J.
• Primary Examiner(s): SHAFER, RICKY D
• Application Number:
  US08/540,736
• Time in Patent Office: 1,084 Days
• Field of Search: 359/198, 359/199, 359/213, 359/214, 359/220, 359/225, 359/221, 359/554, 359/555, 359/402, 359/405, 359/872, 359/874, 359/876, 359/877, 359/900
• US Class Current: 359/214.1
• CPC Class Codes: B60R 1/025 comprising special mechanical means for correcting the field of view in relation to particular driving conditions, e.g. change of lane; scanning mirrors
• CPC Class Codes: G09F 9/313 being gas discharge devices G09F9/302 takes precedence; gas discharge panels comprising a number of discharge gaps per se H01J17/49
• CPC Class Codes: H01J 17/492 with crossed electrodes

Abstract

An articulated viewing apparatus (10) has a pair of elevational actuators (56, 78), one of which is a coarse-position actuator (56) and the other of which is a fine-position actuator (78), and each of which pivots a mirror head (28) about respective parallel elevational axes (54, 66'"'"'). Pivotal movements of the mirror head (28) direct the line of sight of a viewer looking outwardly through a window (22). The window (22) may be formed in the wall of a vehicle or may be at the upper end of a periscope tube, for example, and includes a transparent material (24). This window (22) may admit light to an optical sensor or to the user'"'"'s eye directly. The coarse-position elevational actuator (56) is positioned so that its axis (54) is located as close as possible to an edge of the mirror head (28) and close to the inner surface of the window glazing (24) so that the size of the window (22) is minimized with respect to the size of the optical aperture and field of view provided to the user of the apparatus (10). The fine-position actuator (78) is attached to the mirror head (28) at a respective axis (66'"'"') approximately at the geometric center of the mirror (28), so that the mirror (28) is statically balanced about the fine-position elevation axis (66'"'"') of this actuator (78).

Claims

1. A viewing apparatus for selectively directing the line-of-sight of a viewer, said viewing apparatus comprising:

a mirror for reflecting light from a scene to provide an image of the scene for the viewer;

a support structure pivotally holding said mirror, said support structure including a support arm pivoting near a first end thereof about a support arm pivot axis on said support structure for selectively varying an elevational angle of said mirror relative to the scene, said support arm near an opposite second end thereof supporting said mirror, wherein the weight of said mirror and said support arm exert a mirror torque about said support arm pivot axis;

a counterbalance pivotally connected at a first end thereof to said support structure about a counterbalance pivot axis, wherein the weight of said counterbalance exerts a counterbalance torque about said counterbalance pivot axis, and wherein said support arm pivot axis is substantially parallel to said counterbalance pivot axis; and

a linkage coupling said counterbalance pivot axis to said support arm pivot axis with a flexible belt-like member so that said mirror torque and said counterbalance torque oppose one another upon movement of said mirror.

2. The viewing apparatus of claim 1 wherein said counterbalance includes an arm pivoted on said support structure.

3. The viewing apparatus of claim 1 wherein said counterbalance includes an extended portion adjacent said counterbalance pivot axis and said linkage connects said extended portion with said support arm.

4. The viewing apparatus of claim 3 wherein said support arm includes a corresponding extended portion, and said belt-like member drivingly engages said extended portion of said support arm so that said support arm and said counterbalance arm move in synchronization.

5. The viewing apparatus of claim 1 wherein said counterbalance is generally of hammer shape and includes a relatively enlarged head portion spaced from said counterbalance pivot axis.

6. The viewing apparatus of claim 1 wherein said support arm and said counterbalance move in synchronization with one another in the same direction of angular motion to substantially remain mutually parallel with one another.

7. The viewing apparatus of claim 1 wherein said support structure is also pivotally movable about a vertically oriented azimuthal axis, thereby to provide an user of the viewing apparatus with a line-of-sight also movable in azimuth.

8. The viewing apparatus of claim 1 further including a control system for stabilizing the line of sight of the viewer in opposition to perturbations of said support structure, said control system including a pair of two-axis angular rate sensors each providing a pair of output signals one of which is indicative of an angular rate of said mirror about a respective one of an elevational axis and an azimuthal axis, and the other of which is indicative of angular rate of said mirror about an axis orthogonal to said respective one of said elevational or azimuthal axis.

9. The viewing apparatus of claim 8 wherein said control system includes a pair of angular position sensors each providing a respective output signal indicative of angular position of said mirror.

10. The viewing apparatus of claim 9 wherein said control system includes a loop stabilization calculator providing a feedback signal for use in stabilizing said mirror according to the expression:

##EQU3## in which G is the Laplace transform of the stabilization loop compensation, S is the Laplace operator, K is a gain constant, ω

_z and ω

_p are lead-lag networks, and ω

_i is an integral-lead network, and the servo parameters ω

_z, ω

_p and ω

_i are selected to provide a desired stabilization band width for said viewing apparatus.

11. The viewing apparatus of claim 10 wherein said viewing apparatus further includes a coarse-elevation actuator pivoting said support arm relative to said support structure, and a fine elevation actuator pivoting said mirror relative to said support arm, said control system including a coarse elevation position loop compensator effecting the following relationship for said coarse elevation actuator:

##EQU4## in which G_p (s) is the Laplace transform of the position loop compensation, S is the Laplace operator, K_p is a gain constant, ω

_pz and ω

_pp are lead-lag networks the parameters of which are selected to provide a desired coarse-position loop band width for said viewing apparatus.

12. The viewing apparatus of claim 10 wherein said control system includes circuitry effecting the following relationships among said signals from said pair of two-axis angular rate sensors, and said output signals from said pair of angular position sensors indicative of angular position of said mirror:

space="preserve" listing-type="equation">Elevation Signal.sub.126 =2A.sub.el -A.sub.az2

space="preserve" listing-type="equation">Azimuth Signal.sub.160 =A.sub.az +2 A.sub.el2 sin(E.sub.f +E.sub.c)

in which A_az and A_az2 represents the two output signals from one of said two-axis rate sensors, A_el, and A_el2 represents the two output signals from the other of said two rate sensors, E_f, and E_c represents said output signals from said pair of angular position sensors indicative of angular position of said mirror.

13. A method of operating a viewing apparatus for selectively steering in elevation the line-of-sight of a viewer viewing a scene outwardly through an aperture, said method including steps of:

providing a mirror;

reflecting from said mirror light from said scene which passes inwardly through said aperture to provide an image of said scene to said viewer;

providing a support structure movably holding said mirror for pivotal movement about a horizontal elevational axis;

providing said support structure with apparatus for selectively varying an angle of said mirror about said horizontal elevational axis relative to the scene to selectively steer the viewer'"'"'s line-of-sight in elevation;

providing said support structure with a selectively movable support arm pivoting near a first end thereof on said support structure;

utilizing said support arm to pivotally support said mirror near an opposite second end thereof so that said support arm is undesirably pivotal in response to acceleration of said support structure thereby altering the angle of said mirror and undesirably moving the line-of-sight in elevation;

providing a counterbalance carried on said support structure;

moving said counterbalance in response to said acceleration of said support structure; and

linking said counterbalance to said support arm using a flexible belt-like member so that movement of said counterbalance in response to said acceleration opposes said undesirable pivoting of said support arm and said mirror, thereby to eliminate said undesirable alteration of the angulation of said mirror and undesirable movement of the line-of-sight in elevation.

14. The method of claim 13 further including the steps of:

configuring said counterbalance as an arm member, and

pivoting said counterbalance arm member on said support structure.

15. The method of claim 13 further including the steps of:

using said flexible belt-like member to cause said counterbalance to move in substantial synchronization with said support arm.

16. The method of claim 13 further including the steps of:

using said flexible belt-like member to cause said counterbalance and said support arm to move in synchronization with one another in the same direction of angular motion so as to substantially remain mutually parallel with one another.

17. The method of claim 13 further including the steps of:

configuring said counterbalance to be generally of hammer shape and to include a relatively enlarged head portion spaced from a pivotal connection of said counterbalance with said support structure.

18. A viewing apparatus for selectively directing the line-of-sight of a viewer, said viewing apparatus comprising:

a mirror for reflecting light from a scene to provide an image of a scene for the viewer;

a support structure pivotally holding said mirror, said support structure including a support arm pivoting near a first end thereof about a support arm pivot axis on said support structure for selectively varying an elevational angle of said mirror relative to the scene, said support arm near an opposite second end thereof supporting said mirror, wherein the weight of said mirror and said support arm exert a mirror torque about said support arm pivot axis;

a counterbalance pivotally connected at a first end thereof to said support structure about a counterbalance pivot axis, wherein the weight of said counterbalance exerts a counterbalance torque about said counterbalance pivot axis, and wherein said support arm pivot axis is substantially parallel to said counterbalance pivot axis;

a linkage coupling said counterbalance pivot axis to said support arm pivot axis with a flexible belt-like member so that said mirror torque and said counterbalance torque oppose one another upon movement of said mirror; and

a control system for stabilizing the line of sight of the viewer in opposition to perturbations of said support structure, said control system including a pair of two-axis angular rate sensors each providing a pair of output signals one of which is indicative of an angular rate of said mirror about a respective one of an elevational axis and an azimuthal axis, and the other of which is indicative of an angular rate of said mirror about an axis orthogonal to said respective one of said elevational axis or said azimuthal axis.

19. The viewing apparatus of claim 18 wherein said control system includes a pair of angular position sensors each providing a respective output signal indicative of angular position of said mirror.

20. The viewing apparatus of claim 18 wherein said control system includes a loop stabilization calculator providing a feedback signal for use in stabilizing said mirror according to the expression:

##EQU5## in which G is the Laplace transform of the stabilization loop compensation, S is the Laplace operator, K is a gain constant, ω

_z and ω

_p are lead-lag networks, and ω

_i is an integral-lead network, and the servo parameters ω

_z, ω

_p and ω

_i are selected to provide a desired stabilization band width for said viewing apparatus.

21. The viewing apparatus of claim 20 wherein said control system includes circuitry effecting the following relationships among said signals from said pair of two-axis angular rate sensors, and said output signals from said pair of angular position sensors indicative of angular position of said mirror:

space="preserve" listing-type="equation">Elevation Signal.sub.126 =2A.sub.el -A.sub.az2

space="preserve" listing-type="equation">Azimuth Signal.sub.160 =A.sub.az +2 A.sub.el2 sin(E.sub.f +E.sub.c)

in which A_az and A_az2 represents the two output signals from one of said two-axis rate sensors, A_el, and A_el2 represents the two output signals from the other of said two rate sensors, E_f, and E_c represents said output signals from said pair of angular position sensors indicative of angular position of said mirror.

22. The viewing apparatus of claim 18 wherein said viewing apparatus further includes a coarse-elevation actuator pivoting said support arm relative to said support structure, and a fine-elevation actuator pivoting said mirror relative to said support arm, said control system including a coarse elevation position loop compensator effecting the following relationship for said coarse elevation actuator:

##EQU6## in which G_p (s) is the Laplace transform of the position loop compensation, S is the Laplace operator, K_p is a gain constant, ω

_pz and ω

_pp are lead-lag networks the parameters of which are selected to provide a desired coarse-position loop band width for said viewing apparatus.

23. A rotatable turret for selectively directing the line-of-sight of a viewer within a military vehicle, said turret comprising:

a mirror for reflecting light from a scene to provide an image of the scene for the viewer;

a two or more axis remotely powered articulate support structure pivotally holding said mirror, said support structure including a support arm pivoting near a first end thereof about a support arm pivot axis on said support structure for selectively remotely varying an elevational angle of said mirror relative to the scene, said support arm near an opposite second end thereof supporting said mirror, wherein the weight of said mirror and said support arm exert a mirror torque about said support arm pivot axis;

a coarse actuator remotely controlled by the viewer for driving said mirror about said elevational angle;

a counterbalance pivotally connected at a first end thereof to said support structure about a counterbalance pivot axis, wherein the weight of said counterbalance exerts a counterbalance torque about said counterbalance pivot axis, and wherein said support arm pivot axis is substantially parallel to said counterbalance pivot axis; and

a linkage coupling said counterbalance pivot axis to said support arm pivot axis so that said mirror torque and said counterbalance torque oppose one another upon movement of said mirror.

24. The turret of claim 23 wherein said counterbalance includes an arm pivoted on said support structure.

25. The turret of claim 23 wherein said counterbalance includes an extended portion adjacent said counterbalance pivot axis and said linkage connects said extended portion with said support arm.

26. The turret of claim 23 wherein said support arm and said counterbalance arm move in synchronization with one another in the same direction of angular motion to substantially remain mutually parallel with one another.

27. The turret of claim 23 wherein said support structure is also remotely pivotally movable by the viewer about a vertically oriented azimuthal axis, thereby to provide the viewer with a line-of-sight also movable in azimuth.

28. The turret of claim 23 further including control system for stabilizing the line of sight of the viewer in opposition to perturbations of said support structure, said control system including a pair of two-axis angular rate sensors each providing a pair of output signals one of which is indicative of an angular rate of said mirror about a respective one of an elevational axis or an azimuthal axis, and the other of which is indicative of angular rate of said mirror about an axis orthogonal to said respective one of said elevational or azimuthal axis.

29. The turret of claim 28 wherein said control system includes a pair of angular position sensors each providing a respective output signal indicative of angular position of said mirror.

30. The turret of claim 28 further comprising a fine actuator controlled by said line of sight stabilizing control system for driving said mirror about said elevational angle in opposition to said perturbations.