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- W4366702512 abstract "Space probe is one of the important areas for commercial space industry. In order to make the ion propulsion system have good control performance under the regulation of wide voltage and wide power, a nonlinear controller with adjustable multi-operating points is designed based on the synergetic approach to control (SAC) theory. The duty cycle of DC/DC converter can be calculated by combining the state space equation of DC/DC converter and the evolution law of manifold. In order to ensure that the overshoot of inductor current is small and the response speed is fast when the operating point is switched, according to the convergence characteristics of manifold, the adaptive control parameter is designed based on capacitor voltage error. According to the simulation results, the steady-state error of bus voltage under SAC control is 3.3%, which is less than 6% of PI control. For the transient process of switching, the overshoot of capacitor voltage and inductor current under PI control are close to 30%, much larger than that under SAC control, and the duty cycle under PI control also shows a large oscillation. SAC control has advantages over PI control in terms of steady-state performance, dynamic performance and duty cycle control." @default.
- W4366702512 created "2023-04-24" @default.
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- W4366702512 date "2023-01-01" @default.
- W4366702512 modified "2023-10-18" @default.
- W4366702512 title "Optimization Control of Power Supply for Ion Propulsion System in Multi-operating Points Mode" @default.
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- W4366702512 doi "https://doi.org/10.1007/978-981-99-1576-7_25" @default.
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