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.
Descriptors:
Subject Categories:
- Guided Missile Trajectories, Accuracy and Ballistics
- Rockets