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An analysis of the optimization of a beam rider missile system
- Author / Creator
- Available as
- Online
- Summary
-
A transfer function is derived for a beam rider missile guidance system which is optimum when the target moves in a nonstationary way. The effects of acceleration limiting are considered and a disc...
A transfer function is derived for a beam rider missile guidance system which is optimum when the target moves in a nonstationary way. The effects of acceleration limiting are considered and a discussion of the miss as a function of the various parameters which determine it is included. A form of design chart is presented which allows the immediate determination of the optimum under any set of target-missile conditions.
Details
- Creator
- by Marvin Shinbrot and Grace C. Carpenter
- Format
- Books
- Language
- English
- Contributors
- Publication
-
- Washington : National Advisory Committee for Aeronautics, 1958
- Physical Details
-
- 1 online resource (34 pages) : illustrations
- data file
- OCLC
- on1437556406
- Date of issue: March 1958.
- Report numbers NACA-TN-4145.
- "Ames Aeronautical Laboratory."
- Title from title screen (viewed June, 3, 2024)
- Includes bibliographical references (page 29)
- Electronic reproduction. Denton, Texas : University of North Texas, 2011. Electronic reproduction from print master produced by University of North Texas.