Study is concerned with angular motion of rigid axisymmetrical body having thrust malalignment and another moment due to deflection of control surfaces or control jets; in linear feedback system which is used in control of spin-stabilized space vehicle, preferable combinations of control parameters, such as feedback gain, spin rate, feedback phase difference and damping of system, are obtained to optimize stability and control of vehicle.
Linear dynamic analysis of spinning axisymmetrical rocket or vehicle
Tokyo. Univ -- Inst Space Aeronautical Science -- Report
1965
57 pages
Report
English
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