
Aerospace, Год журнала: 2024, Номер 11(11), С. 920 - 920
Опубликована: Ноя. 8, 2024
Electric power supply (EPS) is the heart of any aerospace mission and plays an important role in improving performance service lifetime spacecraft. It generates, converts, stores, distributes to different voltage levels. The EPS composed solar panels, a conditioning unit (PCU), batteries, distribution (PDU). This paper describes design analysis efficient system for CubeSat standard small satellite. For this purpose, aim propose two-input maximum point tracker (MPPT)-based interleaved boost converter. copes with fact that when satellite revolves around Earth, single panel or at most two panels face radiation angles. In order extract from designed converter drives (MPP). A signal model drawn converter, closed-loop gain analyzed using Bode diagram. To improve phase margin gain, PID compensator added closed loop Finally, proposed validated by simulation results.
Язык: Английский