Closed loop solar array-ion thruster system with power control circuitry

• US 4,143,314 A
• Filed: 03/29/1978
• Issued: 03/06/1979
• Est. Priority Date: 03/29/1978
• Status: Expired due to Term

• Current Assignee: United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration
• Original Assignee: United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration
• Inventors: Gruber, Robert P.
• Primary Examiner(s): Pellinen, A. D.
• Application Number:
  US05/891,370
• Time in Patent Office: 342 Days
• Field of Search: 315/291, 315/308, 325/15, 325/19, 325/20
• US Class Current: 323/288
• CPC Class Codes: G05F 1/67 to the maximum power available from a generator, e.g. from solar cell
• CPC Class Codes: H02J 7/35 with light sensitive cells
• CPC Class Codes: Y02E 10/56 Power conversion systems, e.g. maximum power point trackers

Abstract

A solar array-ion thruster system including a power control circuit which provides for use of the thruster itself in operating the solar array at the maximum power point. The power control circuit is connected between the solar array and the ion thruster and receives voltage and current signals from the former. The control circuit multiplies the voltage and current signals together to produce a power signal which is differentiated with respect to time. The differentiator output is detected by a zero crossing detector and, after suitable shaping, the detector output is phase compared with a clock in a phase demodulator. An integrator receives no output from the phase demodulator when the operating point is at the maximum power point but is driven toward the maximum power point for non-optimum operation. A ramp generator provides minor variations in the beam current reference signal produced by the integrator in order to obtain the first derivative of power.

Claims

1. A power control circuit for a solar array ion thruster system wherein the ion thruster beam current is controlled so as to operate the solar array at the maximum power point, said power control circuit being connected between the solar array and the ion thruster and receiving signals from said solar array corresponding to the solar array current and the solar array voltage, said power control system comprising multiplier means for multiplying together said solar array voltage signal and said solar array current signal to produce a power signal, differentiation means for differentiating said power signal, detector means for determining when the output of said differentiator means lies above and below a predetermined level and for providing an output in accordance therewith, a clock circuit, phase comparator means for comparing the phase of the output of said detector means with the phase of said clock circuit and producing an output in accordance therewith, integrator means for integrating the output of said phase comparator means over a predetermined time period so as to produce an output signal for controlling the ion thruster, and means controlled by said clock circuit for introducing controlled variations on the output signal of the power control circuit so as to ensure that said differentiator means produces an output.

2. A power control circuit as claimed in claim 1 wherein said means for introducing controlled variations in the output signal of the power control circuit comprises a ramp generator connected to said clock circuit.

3. A power control circuit as claimed in claim 2 further comprising a summing amplifier connected to the output of said integrator means and said ramp generator for producing a beam current reference for controlling the ion thruster.

4. A power control circuit as claimed in claim 1 wherein said detector means comprises a zero crossing detector.

5. A power control circuit as claimed in claim 4 further comprising a shaping circuit connected between said zero crossing detector and said phase comparator means.

6. A power control circuit as claimed in claim 3 wherein said detector means comprises a zero crossing detector.