Optical apparatus

Claim 2

In an optical tracking system, lens means defining an optical axis, radiant energy responsive means spaced from said lens means along said optical axis, a pair of radiant energy directing means disposed to be traversed by radiant energy passing along said optical axis from said lens means to said radiant energy responsive means, drive means for simultaneously rotating said radiant energy directing means whereby to rotate a beam of received radiant energy and cause the same to nutate about the optical axis and to trace a substantially circular image upon said radiant energy responsive means, and means for angularly adjusting one of said radiant energy directing means relative to the other to modify the radius of said circular image.

Claim 3

An optical tracking system according to claim 1 and characterized in that said radiant energy directing means comprises a pair of optical prisms.

Claim 4

A tracking system according to claim 1 and characterized in that said last recited means is operable, angularly to adjust said one radiant energy directing means relative to the other at an angular velocity that is a function of the rate of change in range of an object undergoing tracking, said angular velocity being of a value effective to maintain the radius of said circular image at a predetermined substantially fixed value.

Claim 5

A system according to claim 1 and characterized in that said last recited means comprises a differential drive means including: a rotatable shaft; a pair of spaced gears coaxially disposed for rotation upon and with respect to said shaft, one of said gears supporting said one radiant energy directing means and the other of said gears being disposed and adapted for rotation by said drive means; a spider keyed to said shaft; a gear rotatably mounted upon said spider and meshed with said pair of gears in provision of driving connection between said drive means and said one gear; and means for rotating said shaft angularly to position said spider and effect the recited angular adjustment of the one light directing means.

Claim 6

A system according to claim 4, and further characterized in that said means for rotating said shaft comprises: a cam driven by said drive means; and a cam follower coupled with said shaft and operable to rotate the latter.

Claim 7

A system according to claim 1 and characterized in that said radiant energy responsive means comprises a quadrant detector array.

Claim 8

A system according to claim 1 and further characterized in that said last recited means is operable to reposition said one prism relative to the other at a uniformly changing rate of speed.

Claim 9

In combined sighting and tracking apparatus for use in a vehicle to aim and track an energy radiating missile launched therefrom, optical means comprising: means for establishing a line of sight; and a tracking device aligned with the line of sight and including an array of adjacent detectors, a pair of rotatable radiant energy directing means disposed to be traversed by a beam of energy radiated from said missile, and operable to nutate a beam of the radiant energy received from the missile upon said array, and means for rotatably positioning one of said energy directing means relative to the other to control the radius of the traced image in accordance with the change in range of said missile.

Claim 10

In combined sighting and tracking apparatus for use in a vehicle to aim and track an energy radiating missile launched therefrom, optical means comprising: means for establishing a line of sight; and a tracking device aligned with the line of sight and including an array of adjacent detectors, a pair of rotatable radiant energy directing means disposed to be traversed by a beam of energy radiated from said missile, and operable to nutate a beam of the radiant energy received from the missile upon said array, and means for rotatably positioning one of said energy directing means relative to the other to control the radius of the traced image in accordance with the change in range of said missile.

Claim 11

Apparatus according to claim 8 and characterized in that said last recited means is operable to maintain a substantially uniform radius of the traced image.

Claim 12

In combined sighting and tracking apparatus for use in a vehicle to aim and track a missile launched therefrom, optical means comprising: a device for establishing a line of sight; and a tracking device optically aligned with the line of sight and including a screen, a pair of rotatable optical prisms optically aligned with said screen and operable to nutate a beam of the radiant energy received from the missile upon said screen, and means for rotatably positioning one of said prisms relative to the other to establish a beam trace of substantially uniform radius on said screen in accordance with the change in range of said missile.

Claim 13

In combined sighting and tracking apparatus for use in a vehicle to aim and track a missile launched therefrom, optical means comprising: a device for establishing a line of sight; and a tracking device optically aligned with the line of sight and including a screen, a pair of rotatable optical prisms optically aligned with said screen and operable to nutate a beam of the radiant energy received from the missile upon said screen, and means for rotatably positioning one of said prisms relative to the other to establish a beam trace of substantially uniform radius on said screen in accordance with the change in range of said missile.

Claim 14

Apparatus according to claim 9 and characterized in that said screen comprises a quadrant detector array, and in that said last recited means comprises differential adding and subtracting means.

Claim 15

An optical system comprising: an objective lens arranged on an optical axis of the system; a first lens spaced from said objective lens along the optical axis of the system, said first lens having a face presented toward said objective lens and perpendicular to said optical axis and a face opposite to the first disposed with angularity to the optical axis; a second lens spaced from said first lens along the optical axis and having a face angularly disposed as respects the optical axis and facing the angularly disposed face of the said first lens, and a face opposite its angularly disposed face and perpendicular to the optical axis; screen means disposed in the focal plane of the recited lens system for receiving an image of rays entering said objective lens and passing through said first and second lenses; means for rotating said first and second lenses about said optical axis whereby to nutate said image upon said screen means; and means for relatively angularly displacing said first and second lenses to modify the radius of a nutational image directed onto said screen means.

Claim 16

An optical system comprising: an objective lens arranged on an optical axis of the system; a first lens spaced from said objective lens along the optical axis of the system, said first lens having a face presented toward said objective lens and perpendicular to said optical axis and a face opposite to the first disposed with angularity to the optical axis; a second lens spaced from said first lens along the optical axis and having a face angularly disposed as respects the optical axis and facing the angularly disposed face of the said first lens, and a face opposite its angularly disposed face and perpendicular to the optical axis; screen means disposed in the focal plane of the recited lens system for receiving an image of rays entering said objective lens and passing through said first and second lenses; means for rotating said first and second lenses about said optical axis whereby to nutate said image upon said screen means; and means for relatively angularly displacing said first and second lenses to modify the radius of a nutational image directed onto said screen means.

Claim 17

In combined sighting and tracking apparatus for use in a vehicle to aim and track a missile launched therefrom, optical means comprising: a sighting device including reticle means for establishing a line of sight; and a tracking device optically aligned with the line of sight and including a detector array, a pair of rotatable optical prisms optically aligned with and spaced at fixed distances from said array, said prisms being operable to nutate an image of radiant energy received from the missile and directed upon said detector array, and means for rotatably positioning one of said prisms relative to the other to establish a nutational image of substantially uniform size on said detector array upon a change in range of said missile.

Claim 18

In combined sighting and tracking apparatus for use in a vehicle to aim and track a missile launched therefrom, optical means comprising: a sighting device including reticle means for establishing a line of sight; and a tracking device optically aligned with the line of sight and including a detector array, a pair of rotatable optical prisms optically aligned with and spaced at fixed distances from said array, said prisms being operable to nutate an image of radiant energy received from the missile and directed upon said detector array, and means for rotatably positioning one of said prisms relative to the other to establish a nutational image of substantially uniform size on said detector array upon a change in range of said missile.

Claim 19

In combined sighting and tracking apparatus for use in a vehicle to aim and track a missile launched therefrom, optical means comprising: means for establishing a line of sight; and means for tracking optically aligned with the line of sight and including an objective lens, a screen spaced a predetermined fixed distance from said objective lens, and a pair of rotatable optical prisms spaced a fixed distance from said objective lens and optically aligned with the latter and said screen, said prisms being operable to nutate an image of radiant energy received from said missile and directed by said objective lens upon said screen, and means for rotatably positioning one of said prisms relative to the other to establish a nutational image of substantially uniform size on said screen upon the change in range of said missile.

Claim 20

In combined sighting and tracking apparatus for use in a vehicle to aim and track a missile launched therefrom, optical means comprising: means for establishing a line of sight; and means for tracking optically aligned with the line of sight and including an objective lens, a screen spaced a predetermined fixed distance from said objective lens, and a pair of rotatable optical prisms spaced a fixed distance from said objective lens and optically aligned with the latter and said screen, said prisms being operable to nutate an image of radiant energy received from said missile and directed by said objective lens upon said screen, and means for rotatably positioning one of said prisms relative to the other to establish a nutational image of substantially uniform size on said screen upon the change in range of said missile.

Claim 21

In an optical system, an objective lens defining an optical axis of the system, a screen spaced from said lens along the said optical axis and disposed in the focal plane of said lens, a pair of simultaneously rotatable optical prisms optically aligned with and spaced at fixed distances from said objective lens and from said screen, said prisms being cooperable to nutate an image of radiant energy directed by said lens onto said screen, and means for rotatably repositioning one of said prisms relative to the other to modify the radius of the nutated image.

Claim 22

In an optical system, an objective lens defining an optical axis of the system, a screen spaced from said lens along the said optical axis and disposed in the focal plane of said lens, a pair of simultaneously rotatable optical prisms optically aligned with and spaced at fixed distances from said objective lens and from said screen, said prisms being cooperable to nutate an image of radiant energy directed by said lens onto said screen, and means for rotatably repositioning one of said prisms relative to the other to modify the radius of the nutated image.

Claim 23

An optical system according to claim 15, and characterized in that said recited elements comprise tracking means for a heat radiating object moving at a predetermined velocity away from said system, whereby the radius of the nutated image tends to decrease as a function of the distance the object moves away, said system including means for programming the rotatable repositioning of the recited prism relative to the other whereby to maintain the radius of the nutated image at a predetermined desired value.

Claim 24

In an optical tracking system, lens means defining an optical axis, radiant energy responsive means spaced from said lens means along said optical axis, a pair of radiant energy directing means disposed to be traversed by radiant energy passing along said optical axis from said lens means to said radiant energy responsive means, drive means for simultaneously rotating said radiant energy directing means whereby to rotate a beam of received radiant energy and cause the same to rotate about the optical axis and to trace a circular image upon said radiant energy responsive means, and means for effecting differential angular movement of one of said radiant energy directing means relative to the other as they are rotated simultaneously, whereby to modify the radius of said circular image.

Claim 25

In an optical tracking system, lens means defining an optical axis, radiant energy responsive means spaced from said lens means along said optical axis, a pair of radiant energy directing means disposed to be traversed by radiant energy passing along said optical axis from said lens means to said radiant energy responsive means, drive means for simultaneously rotating said radiant energy directing means whereby to rotate a beam of received radiant energy and cause the same to rotate about the optical axis and to trace a circular image upon said radiant energy responsive means, and means for effecting differential angular movement of one of said radiant energy directing means relative to the other as they are rotated simultaneously, whereby to modify the radius of said circular image.

Claim 26

A system according to claim 17 and characterized in that said drive means comprises first and second gear means operable to rotate said radiant energy directing means, said second gear means including a driving gear and a planetary gear train driven thereby, said planetary train being rotatable independently of said driving gear, and thereby operable angularly to move the one radiant energy directing means, to modify the radius of said circular image.