Dynamic equations of motion are developed which describe the rotational motion for a large space structure having rotating appendages. The presence of the appendages produce torque coupling terms which are dependent on the inertia properties of the appendages and the rotational rates for both the space structure and the appendages. These equations were formulated to incorporate into the Space Station Attitude Control and Stabilization Test Bed to accurately describe the influence rotating solar arrays and thermal radiators have on the dynamic behavior of the Space Station.
Space Station Rotational Equations of Motion
1985
21 pages
Report
Keine Angabe
Englisch
Uncontrollable Rotational Motion of the Mir Orbital Station
Springer Verlag | 2001
|Uncontrollable Rotational Motion of the Mir Orbital Station
Online Contents | 2001
|Rotational equations of motion for a triaxial rigid body
AIAA | 1971
|