Thermal analysis of solar array with rigid substrate on spacecraft in orbit;

Method for determining the equivalent capacitance of solar array sample;

An estimative examination to the hedge electrostatic discharge of high voltage and high power solar array;

Research on multi-development and locking mechanism for solar cell array;

In this article, we summarize the shunt technology of solar cell array of spacecraft, and analyze the principle of three kinds of switch shunt regulation technology, namely PWM,S3R and S4R.

Thermally induced vibration of the main mast of the space station s solar arrays;

Based on the solar cell mathematic model,a practical solar array simulator was designed.

Deployment dynamics of solar arrays on ground is simulated by using numerical methods.

Dynamic procedure of deployment of a solar array in the ground environment was simulated by numerical method,where the air influence was regarded as added generalized mass.

The design of an earth observation satellite system with big flexible accessories,such as the solar panel and antenna,and driven by the solar panel,is to suppress the influence of the solar panel drive and flexible vibrations of the solar panel and antenna on the attitude of the satellite.

This circuit gets direct coupling between solar energy cell array and storage battery and adopts low power consume single-chip microcomputer P87LPC767 as core in control circuit.

This circuit gets direct coupling between solar energy cell array and storage battery,adopts low power consume single chip microcomputer P87LPC767 as co.