A hybrid multilevel linear quadratic regulator (ML-LQR) approach was developed and applied to the attitude control of models of the rotational dynamics of a prototype flexible spacecraft and of a typical space platform. Three axis rigid body flexible suspension models were developed for both the spacecraft and the space platform utilizing augmented body methods. Models of the spacecraft with hybrid ML-LQR attitude control and with LQR attitude control were simulated and their response with the two different types of control were compared.
Modular design attitude control system
1982-03-08
Report
No indication
English
Modular Design Attitude Control System
NTIS | 1982
|Modular Design Attitude Control System
NTIS | 1983
|Modular design attitude control system
NTRS | 1983
|Exhibit D modular design attitude control system study
NTRS | 1984
|Exhibit D Modular Design Attitude Control System Study
NTIS | 1984
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