Frequency Analysis of Beam-Rider Turning Rates
Abstract
The differential equation for the theoretical trajectory of a beam-rider missile is derived and solved.
Document Details
- Document Type
- Technical Report
- Publication Date
- Nov 21, 1949
- Accession Number
- AD1211747
Entities
People
- C. E. Corum
- C. L. Jr Key
Organizations
- United States Naval Research Laboratory