Sharp nose lens design using refractive index gradient
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Authors
Amichai, Oded
Subjects
Guided projectiles
missile optics
precision guided munitions
infrared optics
guns
gun launched ramjet
sensors
missile optics
precision guided munitions
infrared optics
guns
gun launched ramjet
sensors
Advisors
Date of Issue
1982-06
Date
1982-06
Publisher
Monterey, California. Naval Postgraduate School
Language
en_US
Abstract
For infrared sensors located at the nose of a missile or a
projectile, an age-old problem occurs. A conflict between
optical quality and aerodynamic drag exists. A new approach
for solving this problem is being developed using gradient
refractive index, GRIN, for lens design. The equations for
lens design incorporating GRIN are formulated for the special
case of spherically symmetrical GRIN. A computer code for designing a GRIN lens and for determining aberrations has
been developed. A different program (LENS) calculates
lens design and lens performance for the case of homogeneous
refractive index. Results of this program provide a check
on the more complex program which includes GRIN. The
computed program calculates the spot diagram for both meridianal
and skew rays. The spot diagram, which is the intersection
of rays with the focal plane, is plotted, and the Oj-j^g
and centroid location of the spot diagram are calculated.
Also a cumulative energy diagram is obtained from the program.
The computer code has been organized to calculate the items
enumerated above for either a circular cone for the inside or
outside surface of the pointed lens. For homogeneous
refractive index, both cases are included in the program
discussed in this report. However, for the GRIN case, only
the complete program for a lens with a conical surface on
the outside is reported here. The alternate case is being
developed by a thesis student.
Features of the computer program include the following: use
of many subroutines for clarity and for easy modification, and
use of program structure for easy integration into an
optimization code.
Sample lens designs and lens performance are presented. The
computer code provides the tools for lens design. Considerables
additional work is needed for selecting the best lens design.
Type
Technical Report
Description
Series/Report No
Department
Identifiers
NPS Report Number
NPS67-82-003CR
Sponsors
The work reported herein was carried out for the
Naval Postgraduate school by Dr. Oded Amichai under Contract Nuinber f0^2 8-81-C-H2 31.
The work presented in this report is m support of the DARPA/AIFS
project. The work is a continuation of earlier research efforts
by several thesis students. An age-old problem is the conflict
between optical quality and aerodynamic performance for infrared
domes. The research may provide a means to circumvent the
problem through use of gradient refractive index. The proiect
on Navy Applications of AIFS is funded by Defense Advanced
Reseat projects Agency and is under the cognizance of Professor
A. E. Fuhs.
Funder
Format
Citation
Distribution Statement
Rights
This publication is a work of the U.S. Government as defined in Title 17, United States Code, Section 101. Copyright protection is not available for this work in the United States.