Application of modular control techniques to the attitude control of a prototype flexible spacecraft and a prototype flexible space platform was further developed by determining numerical values for the physical parameters of a four body approximation of the MSFC/hybrid deployable truss incorporated in the space platform model, generating sensitivity coefficients for the model of the flexible spacecraft, evaluating the changes in the digital computer simulation of the flexible spacecraft resulting from the addition of another rigid body to the model and comparing attitude control effectiveness with actuators on more than one rigid body of the model with that for the case in which the actuators were restricted to one body.
Modular design attitude control system
18.03.1983
Report
Keine Angabe
Englisch
Modular Design Attitude Control System
NTIS | 1983
|Modular design attitude control system
NTRS | 1982
|Modular Design Attitude Control System
NTIS | 1982
|Exhibit D modular design attitude control system study
NTRS | 1984
|Exhibit D Modular Design Attitude Control System Study
NTIS | 1984
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