Abstract: In this brief, a global finite-time adaptive attitude control algorithm is investigated for flexible spacecraft with slosh structure under model uncertainty, external disturbance, and ...
Abstract: A dielectric barrier discharge (DBD) plasma actuator for controlling airflow is proposed. It consists of diverging and converging nozzles, two concentric cylinders, and an actuator mounted ...
Some results have been hidden because they may be inaccessible to you
Show inaccessible results
Feedback