No abstract

The problems, devoted to power quality and particularly power factor correction, are of great importance nowadays. The key requirements, which should be satisfied according to the energy efficiency paradigm, are not limited only by high quality of the output voltage (low total harmonic distortion), but also assume minimal power losses (high efficiency) in the power factor corrector (PFC). It could be satisfied by the use of quasi-resonant pulse converter (QRPC) due to its high efficiency at high switching frequency instead of the classical pulse-width modulated (PWM) boost converter. A dynamic model of QRPC with zero current switching (ZCS) is proposed. This model takes into account the main features of QRPC-ZCS as a link of a PFC closed-loop system (discreteness, sharp changes of parameters over switching period, input voltage impact on the gain). The synthesized model is also valid for conventional parallel pulse converter over an active interval of commutation. The regulator for current loop of PFC was synthesized based on digital filter using proposed model by the criterion of fast acting.

The analysis of electromagnetic processes in power switch of a zero-current switching quasi-resonant pulse converter with parallel resonant circuit is presented in this paper. The analysis performed by stitching equations illustrating change of power switch current and power switch voltage. The obtained results for each switching interval allowed to estimate the overall power dissipation and power losses for all switching intervals.

A comparison of the parameters of the transient characteristics of the module-optimized closed-loop transfer current of the positioning system without taking into account and taking into account the deep pulse-width modulation of the supply voltage of the linear motor. Their essential difference on speed, overregulation, static error is established. A method of optimization according to the criterion of current circuit speed is proposed, which allows to realize its transient characteristic during a finite number of switching intervals of the pulse-width converter. The synthesis of a digital current loop controller is performed, it allows to realize its transient characteristic without over-regulation during a finite number of switching intervals. The results obtained are based on the transfer function of a pulse-width converter, which is a link in the current loop. It is obtained for the case of deep pulse-width modulation based on the statistical linearization of piecewise-linear modulation characteristics of the channels of the pulse-width converter model. The modulation characteristics are obtained as a result of the expansion of the latitude-modular voltage for multiple values of the control coordinate in the Walsh-Fourier series. The number of Walsh functions taken into account depends on the approximation error and the cutoff frequency of the system. References 11, figures 3.

A review of the current state in quadcopters’ flight control systems showed that the electric drives of their propellers are performed according to single-circuit schemes with feedback on rotational speed in which the error in the results of monitoring the angles of roll, pitch, yaw is worked out by a control system with a PI or PID regulator. There is no astaticism load in such systems and the parameters of the current consumed from the on-board battery are not optimized. The consequence of this is a decrease of service life on-board battery and low quality flight control when the load changes. It is proposed to perform the electric drive system of the quadcopter’s screw according to a two-fold integrating structural scheme in which astaticism is provided during perturbations in control and load. A transient speed characteristic based on the optimization results of the double-integration scheme with speed and current circuits in accordance with a symmetrical optimum the parameters of which do not meet the requirements of quadcopter’s high-quality control flight mode was obtained and do not contribute to an increase in the time of using the energy resource of the on-board battery. It is proposed to include additional smoothing differentiating links at its input to eliminate the shortcomings of the obtained transient characteristic of the electric drive system in terms of speed. The parameters of these links were found using the compensation conditions. The obtained transient characteristics of the electric drive system of the quadcopter’s screws in terms of speed and current do not have sudden changes in the adjustable value and do not have overregulation. The result of such parameters in transient characteristics is high-quality control of the quadcopter’s flight mode and an increase in the time of using the energy resource of the on-board battery.