DocumentCode
359144
Title
Missile impact location prediction using noisy range data
Author
Hanson, Matthew ; Tibbetts, Kevin ; Wohlers, Ron ; Hart, Jack D.
Author_Institution
Photon Res. Assoc. Inc., Newton, MA, USA
Volume
3
fYear
2000
fDate
2000
Firstpage
315
Abstract
Predicting the impact location of Theater Ballistic Missile (TBM) RV´s has typically required tracking data from one or more traditional active and/or passive radar systems. When engine thrust terminates at booster engine cutoff (BECO), integration beyond burnout also requires an accurate state vector at the initiation of ballistic flight, and a reasonable estimate of the RV ballistic coefficient. The proposed algorithm requires no traditional radar data, but incorporates a single collector passive IR metric data set, and a slant range data set acquired via a PRA/KTAADN Monocular Passive Ranging (MPR) algorithm. The proposed study using IR metric and MPR data sets demonstrates the accuracy to which handoff state vectors (burnout to ballistic mode) must be known in order to achieve acceptable impact location accuracy´s. The study results demonstrate that using the less accurate (but also less expensive than radar) single collector MPR and IR metric data sets provides sufficient accuracy to produce useful RV impact location predictions
Keywords
ballistics; error analysis; military computing; missile control; prediction theory; radar theory; radar tracking; real-time systems; PRA/KTAADN Monocular Passive Ranging algorithm; Theater Ballistic Missile; accuracy; ballistic coefficient; ballistic flight; burnout to ballistic mode; handoff state vectors; missile impact location; noisy range data; passive IR metric data set; passive radar; single collector MPR; slant range data set; tracking data; Arm; Engines; Laser radar; Lifting equipment; Missiles; Passive radar; Radar detection; Radar tracking; State estimation; Trajectory;
fLanguage
English
Publisher
ieee
Conference_Titel
Aerospace Conference Proceedings, 2000 IEEE
Conference_Location
Big Sky, MT
ISSN
1095-323X
Print_ISBN
0-7803-5846-5
Type
conf
DOI
10.1109/AERO.2000.879861
Filename
879861
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