Accession Number:

ADA018464

Title:

Optimum Attitude Control of Flexible Bodies.

Descriptive Note:

Final rept.,

Corporate Author:

ALABAMA UNIV UNIVERSITY BUREAU OF ENGINEERING RESEARCH

Personal Author(s):

Report Date:

1975-06-01

Pagination or Media Count:

69.0

Abstract:

Although the major development work on VSR Vibration of a Spinning Rocket was previously done, further refinements were made in VSR under this project and the program was used to analyze case studies pertinent to the parameters of interest. A definition of the current capabilities of VSR and its applicability to this project is included.

Subject Categories:

  • Guided Missile Trajectories, Accuracy and Ballistics
  • Rockets

Distribution Statement:

APPROVED FOR PUBLIC RELEASE