An iterative method for finding the transient response of an automatically controlled missile having non-linear stiffness
Contributors: Naval Postgraduate School (U.S.)
Publisher: College of Aeronautics
Published: 1960
Place of publication: Cranfield, England
Language: eng
Subjects: Aeronautics
Notes: Thesis (Dipl.)--College of Aeronautics, Cranfield, England, 1960.

Bibliography: p. 52.

Approved for public release, distribution unlimited.