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
08.03.1982
Report
Keine Angabe
Englisch
Modular Design Attitude Control System
| NTIS | 1983
Modular Design Attitude Control System
| NTIS | 1982
Modular design attitude control system
| NTRS | 1983
Exhibit D Modular Design Attitude Control System Study
| NTIS | 1984
Exhibit D modular design attitude control system study
| NTRS | 1984