초록 ▼

Boresighting systems and methods are disclosed. In one embodiment, an assembly adapted for boresighting a launch system includes first and second elongated members adapted to be coupled to the launch system. First and second alignment members are coupled to and extend between the first and second el

Boresighting systems and methods are disclosed. In one embodiment, an assembly adapted for boresighting a launch system includes first and second elongated members adapted to be coupled to the launch system. First and second alignment members are coupled to and extend between the first and second elongated members and are adapted to position the elongated members in a substantially aligned, spaced-apart relationship. A mirror assembly is coupled to each elongated member, the mirror assemblies being adapted to provide an average angular position resulting in a single corrector value for the launch system. In a particular embodiment, each of the first and second elongated members is sized to simulate a Stinger missile.

대표청구항 ▼

What is claimed is: 1. An assembly adapted for boresighting a launch system, comprising: a measurement system having a processor; first and second elongated members configured to be coupled to the launch system; first and second alignment members coupled to and extending between the first and secon

What is claimed is: 1. An assembly adapted for boresighting a launch system, comprising: a measurement system having a processor; first and second elongated members configured to be coupled to the launch system; first and second alignment members coupled to and extending between the first and second elongated members and configured to position the elongated members in a substantially aligned, spaced-apart relationship; and a mirror assembly coupled to each elongated member, the mirror assemblies being configured to provide input to the processor, the processor being configured to determine, based on the input, an average angular position resulting in a single corrector value for the launch system, wherein the single corrector value is provided to the launch system for boresighting the launch system. 2. The assembly of claim 1, wherein each of the first and second elongated members includes a substantially-cylindrical body having a plurality of interface locations configured to be coupled to the launch system. 3. The assembly of claim 2, wherein at least one interface location comprises an annular band having a relatively larger diameter than a diameter of an adjacent portion of the substantially-cylindrical body. 4. The assembly of claim 1, wherein each alignment member includes an enlarged end coupled to a first one of the elongated members and a cylindrical end coupled to another of the elongated members. 5. The assembly of claim 1, wherein each mirror assembly includes a first mirror facing a first direction that is substantially parallel with a longitudinal axis of its associated elongated member, and a second mirror facing a second direction that is not parallel with the longitudinal axis. 6. The assembly of claim 5, wherein the first direction intersects the second direction. 7. A missile launch system, comprising: a base configured to be coupled to a launch platform, the based having a plurality of attachment devices configured to be coupled to at least one missile; an adapter assembly for sighting the base, the adapter assembly including: a measurement system having a processor; first and second elongated members configured to be coupled to the attachment devices of the base; first and second alignment members coupled to and extending between the first and second elongated members and configured to position the elongated members in a substantially aligned, spaced-apart relationship; and a mirror assembly coupled to each elongated member, the mirror assemblies being configured to provide input to the processor, the processor being configured to determine, based on the input, an average angular position resulting in a single corrector value for the missile launch system, wherein the single corrector value is provided to the launch system for boresighting the launch system. 8. The system of claim 7, wherein each of the first and second elongated members includes a substantially-cylindrical body having a plurality of interface locations configured to be coupled to the launch system. 9. The system of claim 8, wherein at least one interface location comprises an annular band having a relatively larger diameter than a diameter of an adjacent portion of the substantially-cylindrical body. 10. The system of claim 7, wherein each alignment member includes an enlarged end coupled to a first one of the elongated members and a cylindrical end coupled to another of the elongated members. 11. The system of claim 7, wherein each mirror assembly includes a first mirror facing a first direction that is substantially parallel with a longitudinal axis of its associated elongated member, and a second mirror facing a second direction that is not parallel with the longitudinal axis. 12. The system of claim 11, wherein the first direction intersects the second direction. 13. A method of sighting a launch system, comprising: engaging a first tube member of an adapter assembly with the launch system; engaging a second tube member of the adapter assembly with the launch system; adjusting a first position of the first tube member relative to the second tube member; securing the first tube member into the first position with respect to the launch system; adjusting a second position of the second tube member relative to the first tube member; securing the second tube member into the second position with respect to the launch system; performing measurements of at least one of the first and second positions; determining a corrector value based on the measurements of the at least one of the first and second positions; and boresighting the launch system using the single corrector value. 14. The method of claim 13, wherein engaging a first tube member of an adapter assembly with the launch system includes engaging an upper tube member of an adapter assembly with the launch system. 15. The method of claim 13, wherein engaging a second tube member of an adapter assembly with the launch system includes engaging an lower tube member of an adapter assembly with the launch system. 16. The method of claim 13, wherein at least one of adjusting a first position of the first tube member and adjusting a second position of the second tube member includes adjusting a position of a one of the tube members so that an end portion projecting outwardly from the one of the tube members is positioned tangent to the other of the tube members. 17. The method of claim 13, wherein at least one of securing the first tube member and securing the second tube member includes securing a plurality of clamps of the launch system. 18. The method of claim 13, wherein performing measurements of at least one of the first and second positions includes performing measurements of both the first and second positions. 19. The method of claim 13, wherein performing measurements of at least one of the first and second positions includes performing measurements of at least one of an elevation value, an azimuth value, and a roll value. 20. The method of claim 13, wherein determining a corrector value based on the measurements of the at least one of the first and second positions includes at least one of averaging the measurements and comparing the measurements with a predetermined value to determine the corrector value.