Accession Number : AD0782021
Title : Terminal Miss Sensitivity of a Radar Guided Air-to-Air Missile System.
Descriptive Note : Master's thesis,
Corporate Author : AIR FORCE INST OF TECH WRIGHT-PATTERSON AFB OHIO SCHOOL OF ENGINEERING
Personal Author(s) : Kjesbo,Lee A.
Report Date : JUN 1974
Pagination or Media Count : 112
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)
Descriptors : *Air to air missiles, *Miss distance, Radar homing, Guided missile trajectories, Terminal guidance, Automatic pilots, Mathematical models, Computer programs, Theses
Subject Categories : Guided Missile Traj, Accuracy and Ballistics
Air- and Space-launched Guided Missiles
Distribution Statement : APPROVED FOR PUBLIC RELEASE