loading page

Analysis on the angular jamming effects of electronically controlled corner reflectors towing after a maneuver aircraft
  • +1
  • Lin Gan,
  • Zehao Wu,
  • Jianbing Li,
  • Xuesong Wang
Lin Gan
National University of Defense Technology

Corresponding Author:ganlin16@nudt.edu.cn

Author Profile
Zehao Wu
National University of Defense Technology
Author Profile
Jianbing Li
State Key Laboratory of Complex Electromagnetic Environment Effects on Electronics and Information System (CEMEE),
Author Profile
Xuesong Wang
National University of Defense Technology
Author Profile

Abstract

In this letter, the angular jamming effect of electronically controlled corner reflectors after a maneuver aircraft is analyzed. Motion characteristics of the corner reflectors towed by a high-speed aircraft are calculated through the Lagrange theory, and the angle measurement error of the jamming method for the monopulse angle measurement algorithm is analyzed based on the motion states and the electromagnetic states (scattering or penetration) of the corner reflectors. Results show that the measured angle by a monopulse radar seeker can be effectively interfered by this method under complex maneuver motion while the automatic tracking is employed.
22 Aug 2022Submitted to Electronics Letters
22 Aug 2022Submission Checks Completed
22 Aug 2022Assigned to Editor
24 Aug 2022Reviewer(s) Assigned
01 Oct 2022Review(s) Completed, Editorial Evaluation Pending
04 Oct 2022Editorial Decision: Revise Minor
04 Oct 20221st Revision Received
04 Oct 2022Submission Checks Completed
04 Oct 2022Assigned to Editor
04 Oct 2022Review(s) Completed, Editorial Evaluation Pending
09 Oct 2022Editorial Decision: Accept