DocumentCode
3201812
Title
Neural prediction of missile dynamics during hardware-in-the-loop captive-carry experiments
Author
Gill, C.W. ; Pace, P.E.
Author_Institution
Center for Joint Services Electron. Warfare, Naval Postgraduate Sch., Monterey, CA, USA
Volume
4
fYear
1997
fDate
9-12 Jun 1997
Firstpage
2208
Abstract
The Naval Research Laboratory´s P-3 captive-carry correlation algorithms combine hardware-in-the-loop missile simulator closed-loop anechoic chamber results and open-loop field test results to calculate a single measure of electronic attack effectiveness (miss distance). Prediction of the missile dynamics from the open-loop captive-carry seeker response represents an important component of these algorithms. This paper reports the use of neural networks to predict the missile dynamics by training Levenburg-Marquardt type predictors with the closed-loop seeker azimuth, elevation and range as inputs, the change in position of the missile in spherical coordinates (relative to the missile body), and the missile yaw and pitch as outputs. The trained networks are then used to process the open-loop seeker information to predict the dynamics. The performance of the predictors is evaluated numerically using recent test results. The prediction error is also quantified
Keywords
dynamics; iterative methods; learning (artificial intelligence); military computing; missiles; neural nets; optimisation; parameter estimation; Levenburg-Marquardt type predictors; Naval Research Laboratory; P3 captive-carry correlation algorithm; closed-loop seeker; iterative method; missile dynamics; neural networks; neural prediction; open-loop seeker; optimisation; Aerospace electronics; Aerospace simulation; Aircraft; Anechoic chambers; Computational modeling; Computer simulation; Electronic equipment testing; Electronic warfare; Missiles; Open loop systems;
fLanguage
English
Publisher
ieee
Conference_Titel
Neural Networks,1997., International Conference on
Conference_Location
Houston, TX
Print_ISBN
0-7803-4122-8
Type
conf
DOI
10.1109/ICNN.1997.614282
Filename
614282
Link To Document