A programmable optical system that dynamically corrects or induces aberrations into the optical path of a missile seeker. The system is dynamic in that the amount and type of aberration may be changed while the missile is in flight. The dynamic correction is accomplished by means of deformations applied to a low-mass mirror or mirrors in the optical path of the missile seeker. The missile includes an aspheric dome, and the optical system is dynamically compensated for aberrations introduced by the dome as the seeker system is moved through the field of regard.
申请公布号
DK0941497(T3)
申请公布日期
2003.03.24
申请号
DK19980956092T
申请日期
1998.10.01
申请人
RAYTHEON COMPANY
发明人
CROWTHER, BLAKE, C.;MCKENNEY, DEAN, B.;SPARROLD, SCOTT;JAMES, MILLS;BEARD, DOUGLAS, M.;HARRISON, DANIEL, C.;MILLS, JAMES P.