Terminal Miss Sensitivity of a Radar Guided Air-to-Air Missile System.

Abstract

A terminal miss sensitivity analysis was performed for a linearized, time invariant missile system in a two dimensional plane. First the missile system equations were derived including target modeling, seeker modeling and proportional guidance law modeling. A computer program was written to determine the sensitivity of terminal miss to aberration error slope, target bandwidth and RMS acceleration, and noise bandwidth and RMS magnitude. The RMS acceleration of the target was found to have the greatest effect and aberration error slope the least. (Author)

Document Details

Document Type
Technical Report
Publication Date
Jun 01, 1974
Accession Number
AD0782021

Entities

People

  • Lee A. Kjesbo

Organizations

  • Air Force Institute of Technology

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Bandwidth
  • Computer Programs
  • Computers
  • Equations
  • Guidance
  • Mathematics
  • Physical Properties
  • Sensitivity
  • Terminals
  • Two Dimensional

Fields of Study

  • Physics

Readers

  • Control Systems Engineering.
  • Radar Systems Engineering.