A low-loss, high reliability integration magnetic levitation flywheel DC brushless motor control system
A DC brushless and control system technology, applied in the field of excitation or armature current control, electronic commutator, etc., can solve problems such as difficult to meet the energy supply of spacecraft, unable to achieve high integration design, and reduce system reliability. To achieve the effect of improving anti-interference ability, improving integration and reliability, and improving reliability
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[0031]As shown in Figure 1, the present invention is mainly made up of FPGA system 1, interface circuit 4, position sensor interface circuit 5, power module 8, current detection feedback module 12, wherein FPGA system 1 comprises: hardware circuit part and in FPGA chip based on The control algorithm implemented by hardware programming is composed of a hardware circuit part consisting of an FPGA chip and a corresponding power supply configuration chip. The control algorithm implemented based on hardware programming in the FPGA chip includes: position and speed calculation algorithm 2, software phase-locked loop algorithm 17 , Current regulation algorithm 16, PWM pulse generation algorithm 15, step-down chopper PWM pulse generation algorithm 18, AD control algorithm 14. The power module 8 is composed of five parts including a back EMF peak voltage feedback interface circuit 6 , a step-down chopper module 7 , a high-speed optocoupler isolation circuit 19 , a drive circuit 20 , and...
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