MISSILE TRACKING FROM SHOCK RECORDINGS

MISSILE TRACKING FROM SHOCK RECORDINGS

Equations are developed for determining the speed and direction of motion of a supersonic missile in terms of the times of arrival of the shock at various microphones. Three or more microphones must be placed along the x, y and z axes at each of three or more stations. (Author)

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Bibliographische Detailangaben
1. Verfasser: Reid, Walter P
Format: Report
Sprache:eng
Schlagworte:
ACOUSTIC DETECTION
Acoustics
DIRECTION FINDING
EQUATIONS OF MOTION
ERRORS
GUIDED MISSILE TRACKING SYSTEMS
Guided Missiles
MATHEMATICAL ANALYSIS
MICROPHONES
SHOCK WAVES
TRIANGULATION
VELOCITY
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Beschreibung
Zusammenfassung:Equations are developed for determining the speed and direction of motion of a supersonic missile in terms of the times of arrival of the shock at various microphones. Three or more microphones must be placed along the x, y and z axes at each of three or more stations. (Author)