@article{oai:jaxa.repo.nii.ac.jp:00034380,
 author = {AZUMA, Akira},
 issue = {8},
 journal = {ISAS report/Institute of Space and Aeronautical Science,University of Tokyo},
 month = {Dec},
 note = {This report contains a dynamic analysis of the angular behavior of a spinning body flying either in vacuum or in atmosphere. The study is mainly concerned with the angular motion of a rigid axisymmetrical body having a thrust malalignment and another moment due to the deflection of control surfaces or control jets. In linear feedback system which is used in the control of spin-stabilized space vehicle, preferable combinations of the control parameters, such as feedback gain, spin rate, feedback phase difference and damping of the system, are obtained to optimize the stability and control of the vehicle. In the case of asymmetrical feedback system the linear approximate solution has been obtained. The analysis of the feedback system will be applied to the motion of either launching or re-entry vehicle within atmosphere., 資料番号: SA2400510000},
 pages = {217--273},
 title = {Linear Dynamic Analysis of the Spinning Axisymmetrical Rocket or Vehicle},
 volume = {30},
 year = {1965}
}