Feasibility Analysis for Predicting A Kinetic Kill Zone for Aircraft Homing Missile Defense

reportActive / Technical Report | Accession Number: ADA278705 | Open PDF

Abstract:

An extended Kalman filter is used to predict a kinetic kill zone for use in aircraft self-defense versus homing missiles.

Author(s):
Ennis, Mark E.
Author Organization(s):
AIR FORCE INST OF TECH WRIGHT-PATTERSON AFB OH SCHOOL OF ENGINEERING
Descriptive Note:
Master's thesis
Pagination:
0372

Security Markings

DOCUMENT & CONTEXTUAL SUMMARY

Distribution:
Approved For Public Release
Distribution Statement:
Approved For Public Release; Distribution Is Unlimited.

RECORD

Collection: TR
Identifying Numbers
Report Number(s):
AFIT/GE/GEO-94M-01
Monitor Series:
WL/WP
 Subject Terms
Joint Capability Areas:
JCA_5_Command and Control; JCA_5.3_Planning; JCA_5.5.1_Communicate Intent and Guidance; JCA_5.5_Direct; JCA_1.2.5_Lessons Learned; JCA_4.1_Deployment and Distribution; JCA_5.2.2_Develop Knowledge and Situational Awareness; JCA_5.2_Understand; JCA_4.6_Engineering
Modernization Areas:
Space
Communities of Interest:
Weapons Technologies
Descriptor(s):
*ANTIAIRCRAFT MISSILES, SIMULATION, THESES, GUIDANCE, NOISE, HOMING
Field(s)/Group(s):
Antimissile Defense Systems
Report Date:
1994 Mar 01