Exact(1)
For the illustrative examples the physical model of liquid monopropellant rocket motor with a pressure feeding system and the problem of controlling the yaw angles of a satellite system with delays are considered along with their numerical simulations to show effectiveness of derived results.
Similar(59)
Additionally, within Matlab/Simulink environment, the transient simulation of DFWPG system is carried out and the effectiveness of controller derived in this paper is verified, by comparisons of response effects with PI control and regulation performances under different wind speeds.
The effectiveness of the derived models is illustrated by means of two- and three-dimensional examples.
Finally, three numerical studies are provided to illustrate the accuracy and effectiveness of the derived methods.
Finally, two numerical examples are exploited to show the effectiveness of the derived LMI-based conditions.
Numerical simulations are provided to verify the correctness and effectiveness of the derived theoretical results.
Finally, some numerical simulations are given to demonstrate the effectiveness of the derived theoretical results.
Finally, three numerical examples are provided to demonstrate the effectiveness of the derived theoretical results.
Illustrative numerical examples are provided to demonstrate the effectiveness of the derived results.
Finally, two simulation examples are provided to demonstrate the effectiveness of the derived method.
Moreover, numerical illustrations are provided to validate the effectiveness of the derived analytical results.
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