Claims Analysis
Total Claims: 12
Claim 1
Independent Claim
122 words
An optical sight for identifying an object from an aircraft and measuring the range and bearing to the object from the aircraft comprising: a cabinet; an optical viewer mounted in said cabinet for use in locating an object; image stabilization means mounted in said cabinet and operable to produce a stabilized identifiable image of the object located and positioned with respect to said viewer such that the stabilized image may be observed through said viewer; means mounted in said cabinet for measuring the bearing to the object as sighted through said viewer from the aircraft; and means mounted in said cabinet and connected to said bearingmeasuring means for calculating the range to the object from the aircraft after two successive bearing measurements.
Claim 2
Dependent Claim
122 words
An optical sight for identifying an object from an aircraft and measuring the range and bearing to the object from the aircraft comprising: a cabinet; an optical viewer mounted in said cabinet for use in locating an object; image stabilization means mounted in said cabinet and operable to produce a stabilized identifiable image of the object located and positioned with respect to said viewer such that the stabilized image may be observed through said viewer; means mounted in said cabinet for measuring the bearing to the object as sighted through said viewer from the aircraft; and means mounted in said cabinet and connected to said bearingmeasuring means for calculating the range to the object from the aircraft after two successive bearing measurements.
Claim 3
Dependent Claim
18 words
An optical sight for identifying an object, as in claim 1, wherein said bearing-measuring means comprises a potentiometer
Claim 4
Dependent Claim
18 words
An optical sight for identifying an object, as in claim 1, wherein said bearing-measuring means comprises a gyroscope.
Claim 5
Dependent Claim
32 words
An optical sight for identifying an object, as in claim 1, wherein said image stabilization means utilizes a closed-circuit television system for presenting an electronically enhanced stabilized image of the object identified.
Claim 6
Dependent Claim
21 words
An optical sight for identifying an object, as in claim 4, further comprising a dichroic mirror mounted in said optical viewer
Claim 7
Dependent Claim
21 words
An optical sight for identifying an object, as in claim 5, wherein said optical viewer has a wide angle of view.
Claim 8
Dependent Claim
36 words
An optical sight for identifying an object, as in claim 6, wherein said image stabilization means utilizes first and second gyroscopes for stabilizing the optical image of the object sighted about the x and y axis.
Claim 9
Dependent Claim
18 words
An optical sight for identifying an object, as in claim 7, wherein said range-calculating means is a computer.
Claim 10
Dependent Claim
135 words
An optical sight for identifying an object, as in claim 8, wherein said computer comprises: means connected to said bearing-measuring means for obtaining the sine of angle A, where A is a first bearing from the aircraft to the object sighted; means connect to said bearing means for obtaining the sine of angle B-A where B is a second bearing from the aircraft to the object sighted taken after the aircraft has flown a distance Z from the point at which the first bearing was taken; means for multiplying the sine of angle A by the distance Z; dividing means connected to said multiplying means and said means for obtaining the sine of the angle B-A to divide Z sin A by sin (B-A) to obtain the range of the object identified to the target.
Claim 11
Dependent Claim
18 words
An optical sight for identifying an object as in claim 4, wherein said range-calculating means is a computer.
Claim 12
Dependent Claim
136 words
An optical sight for identifying an object, as in claim 5, wherein said computer comprises means connected to said bearing-measuring means for obtaining the sine of angle A, where A is a first bearing from the aircraft to the object sighted; means connected to said bearing-measuring means for obtaining the sine of angle B-A, where B is a second bearing from the aircraft to the object sighted taken after the aircraft has flown a distance Z from the point at which the first bearing was taken; means for multiplying the sine of angle A by the distance Z; dividing means connected to said multiplying means and said means for obtaining the sine of the angle B-A to divide Z sin A by the sin (B-A) to obtain the range of the object identified to the target.