Full shunt boost switching voltage limiter for solar panel array

Claim 2

A bus voltafie limiter connected between a spacecraft power source, which power source provides a substantially constant current and variable voltage, and a load, said bus voltage limiter connecting said power source to said load and comprising: a coupled inductor having a plurality of windings including at least first and second windings, a switch adapted to be placed in a first state to conduct all current from said power source to said first winding and adapted to be placed in a second state wherein current from said power source flows through said second winding to said load, whereby the output voltage of said power source is varied to maintain output power to said load substantially equal to input power from said power source.

Claim 3

The invention defined in claim 1 wherein said coupled inductor further includes a third winding connected with said source through a second inductor and a dc blocking capacitor and is effective to produce cancellation of input ripple current resulting from operation of said switch.

Claim 4

The invention defined in claim 1 wherein said limiter includes a modulator for controlling the duty cycle of said switch by decreasing the duty cycle in response to increases in load current and by increasing the duty cycle of said switch in response to decreases in load current, to maintain a substantially constant output voltage at said load.

Claim 5

The invention defined in claim 1 wherein said power source comprises an array of solar panels.

Claim 6

The invention defined in claim 4 wherein said switch is a power MOSFET device.

Claim 7

A bus voltage limiter adapted to be connected between a load and a spacecraft power source, which power source is comprised of an array of solar panels providing a substantially constant current and a variable voltage, said limiter comprising: power switch means connected with said power source, a coupled inductor having first and second windings, each winding having first and second ends, an output capacitor connected across said load and to said first end of said first and second windings, an energy transfer capacitor connected to said second end of said first and second windings, said power switch means adapted to connect said second end of said first winding to said source, a diode connecting said second end of said second winding to said source, modulator means for decreasing the duty cycle of said switch means in response to increases in load current and for increasing the duty cycle of said switch means in response to decreases in load current, to maintain a substantially constant output voltage at said load.

Claim 8

A bus voltage limiter adapted to be connected between a load and a spacecraft power source, which power source is comprised of an array of solar panels providing a substantially constant current and a variable voltage, said limiter comprising: power switch means connected with said power source, a coupled inductor having first and second windings, each winding having first and second ends, an output capacitor connected across said load and to said first end of said first and second windings, an energy transfer capacitor connected to said second end of said first and second windings, said power switch means adapted to connect said second end of said first winding to said source, a diode connecting said second end of said second winding to said source, modulator means for decreasing the duty cycle of said switch means in response to increases in load current and for increasing the duty cycle of said switch means in response to decreases in load current, to maintain a substantially constant output voltage at said load.

Claim 9

The invention defined in claim 6 wherein said coupled inductor further includes a third winding connected with said array of solar panels through a second inductor and a dc blocking capacitor and is effective to produce cancellation of input ripple current resulting from operation of said power switch.