2個のホイールによる人工衛星のフィードバック姿勢制御 [in Japanese] Feedback Attitude Control of Spacecraft by Two Wheels [in Japanese]
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The feedback control of attitude changes for a spacecraft with two reaction wheels is considered. Rodriguez parameters are used for attitude expression, and the system is expressed in a simple non-holonomic form. Then a continuous feedback law is proposed for the three-axis control of spacecraft attitude. The stability of the closed-loop system is examined by an equivalent linearized system. The validity of the control law is verified by numerical simulations.
- Transactions of the Institute of Systems, Control and Information Engineers
Transactions of the Institute of Systems, Control and Information Engineers 12(12), 747-753, 1999-12-15
THE INSTITUTE OF SYSTEMS, CONTROL AND INFORMATION ENGINEERS (ISCIE)