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Paths of Target Seeking Missiles in Two DimensionsParameters that enter into equation of trajectory of a missile are discussed. Investigation is made of normal pursuit, of constant, proportional, and line--of-sight methods of navigation employing target seeker, and of deriving corresponding pursuit paths. Pursuit paths obtained under similar conditions for different methods are compared. Proportional navigation is concluded to be best method for using target seeker installed in missile.
Document ID
20090033671
Acquisition Source
Legacy CDMS
Document Type
Other
External Source(s)
hdl:http://handle.dtic.mil/100.2/ADA800542
Authors
Watkins, Charles E. (National Advisory Committee for Aeronautics. Langley Aeronautical Lab. Langley Field, VA, United States)
Date Acquired
August 24, 2013
Publication Date
July 1, 1946
Subject Category
Communications And Radar
Report/Patent Number
ATI No. 4831
NACA-ACR-L6B06
AD-A800542
Report Number: ATI No. 4831
Report Number: NACA-ACR-L6B06
Report Number: AD-A800542
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
ATI-004831
ATI COLLECTION
FLIGHT PATHS
GUIDED MISSILE TRAJECTORIES

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