Abstract:

The evaluation method of the profile error for a radome on vehicles or missiles is studied by use of the saddle point programming(SPP). A linear saddle point programming (LSPP) model applicable to evaluation of radome profile error and minimum condition of evaluation are given. At last, the actual processing method and evaluation examples are presented. It is shown that good results are obtained by using the method in this paper.

Key words: pr ofile er r or evalua tion, radome, saddle-point pr ogramming