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The interconversion of attitude deviations of aerospacecraft during large attitude flight
Pages: 1-10
Year: Issue:  1
Journal: Aerospace Control

Keyword:  Subject termsGround to ground missileLaunch vehicleAttitude control system;
Abstract: In this paper the research of the relations among attitude angles, frame angles and rotation angles, particularly between their deviations, is presented. Frame angles are measured from inertial stabilizing platforms mounted on in ground-to-ground ballistic missile and launch vehicle. Therefore the theoretical basis is established to implement correctlg attitude deviation feedbacks and particularly the large attitude control.
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