导航
ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 2001, Vol. 22 ›› Issue (6): 517-520.
Previous Articles Next Articles
LIU Jun
Received:
Revised:
Online:
Published:
Abstract:
An approach for modeling the missile radome error based on discrete Fourier transform is presented in this paper. The output of a seeker mounted in the missile caused by the radome error is gathered by the semi physical simulation system, and the model of the radome error is calculated. The test for compensating for the radome error has been done, which is based on the highly precise modeling.
Key words: radome, line of sigh t, erro r, Fourier t ransfo rm, compensat ion, sem i-physical simulat ion
LIU Jun. APPROACH FOR MODELING MISSILE RADOME ERROR BASED ON DISCRETE FOURIER TRANSFORM[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2001, 22(6): 517-520.
0 / / Recommend
Add to citation manager EndNote|Reference Manager|ProCite|BibTeX|RefWorks
URL: https://hkxb.buaa.edu.cn/EN/
https://hkxb.buaa.edu.cn/EN/Y2001/V22/I6/517