Systems and methods for performing shape estimation using sun sensors in large-scale space-based solar power stations

• US 10,454,565 B2
• Filed: 08/10/2016
• Issued: 10/22/2019
• Est. Priority Date: 08/10/2015
• Status: Active Grant

• Current Assignee: California Institute of Technology
• Original Assignee: California Institute of Technology
• Inventors: Pellegrino, Sergio, Hajimiri, Seyed Ali, Atwater, Harry A., Talon, Thibaud
• Primary Examiner(s): Aminzay, Shaima Q
• Application Number:
  US15/233,776
• Publication Number:
  US 20170047987A1
• Time in Patent Office: 1,168 Days
• Field of Search: 455 134
• CPC Class Codes: B64G 1/428 Power distribution and management
• CPC Class Codes: B64G 1/4282 for transmitting power to earth or other spacecraft
• CPC Class Codes: H02S 40/30 Electrical components
• CPC Class Codes: H03F 1/0261 with control of the polarisation voltage or current, e.g. gliding Class A
• CPC Class Codes: H03F 2200/451 the amplifier being a radio frequency amplifier
• CPC Class Codes: H03F 2200/462 the current being sensed
• CPC Class Codes: H03F 2200/471 the voltage being sensed
• CPC Class Codes: H03F 2203/45731 the LC comprising a transformer
• CPC Class Codes: H03F 3/19 with semiconductor devices only
• CPC Class Codes: H03F 3/245 with semiconductor devices only
• CPC Class Codes: H03F 3/45183 Long tailed pairs H03F3/4521, H03F3/45237 take precedence
• CPC Class Codes: H03F 3/45192 Folded cascode stages
• CPC Class Codes: H03F 3/68 Combinations of amplifiers, e.g. multi-channel amplifiers for stereophonics power amplifiers using a combination of several semiconductor amplifiers H03F3/211; combinations of amplifiers using coupling networks with distributed constants H03F3/602
• CPC Class Codes: H04B 7/0617 for beam forming
• CPC Class Codes: H04B 7/18513 Transmission in a satellite or space-based system
• CPC Class Codes: H04L 25/085 Arrangements for reducing interference in line transmission systems, e.g. by differential transmission
• CPC Class Codes: H04L 27/152 using controlled oscillators, e.g. PLL arrangements
• CPC Class Codes: H04L 27/261 Details of reference signals
• CPC Class Codes: Y02D 30/70 in wireless communication networks
• CPC Class Codes: Y02E 10/50 Photovoltaic [PV] energy

Abstract

A space-based solar power station, a power generating satellite module and/or a method for collecting solar radiation and transmitting power generated using electrical current produced therefrom is provided. Power transmitters can be coordinated as a phased array and the power generated by the phased array is transmitted to one or more power receivers to achieve remote wireless power generation and delivery. In many embodiments, a reference signal is distributed within the space-based solar power station to coordinate the phased array. In several embodiments, determinations of the relative locations of the antennas in the array are generated by an array of sun sensors that estimate the shape of the module to evaluate the phase shift and/or amplitude modulation to apply to the reference signal at each power transmitter.

Claims

1. A space-based solar power station comprising:

a plurality of unconnected satellite modules disposed in space in an orbital array formation;

a plurality of power generation tiles disposed on and forming an independent array on each of the plurality of satellite modules;

at least one photovoltaic cell disposed on each of the power generation tiles; and

at least one power transmitter collocated with the at least one photovoltaic cell on each of the power generation tiles and in signal communication therewith such that an electrical current generated by the collection of solar radiation by the at least one photovoltaic cell powers the at least one power transmitter, where each of the at least one power transmitters comprises;

an antenna; and

separate control electronics that independently control, based on information from other power generation tiles within the independent array, at least the phase of a radio frequency power signal that feeds the antenna so that the power transmitter is coordinated with power transmitters on other power generation tiles on the plurality of unconnected satellite modules to form a phased array; and

at least one sun sensor disposed on each of the satellite module that is in signal communication with a microcontroller, where the microcontroller is in signal communication with the control electronics in each of the at least one power transmitter and provides a phase offset signal to the control electronics in each of the at least one power transmitter based upon at least one signal received from the at least one sun sensor.

2. The space-based solar power station of claim 1, wherein the control electronics further controls the amplitude of the radio frequency power signal that feeds the antenna so that the power transmitter is coordinated with power transmitters on other power generation tiles.

3. The space-based solar power station of claim 1, wherein:

the power transmitter is configured to receive a reference signal; and

the control electronics controls the phase of the radio frequency power signal by applying a phase shift with respect to the received reference signal.

4. The space-based solar power station of claim 3, wherein at least one of the satellite modules comprises a receiver to wirelessly receive the reference signal.

5. The space-based solar power station of claim 4, wherein the receiver of the at least one satellite module is configured to wirelessly receive the reference signal from an Earth-based transmitter.

6. The space-based solar power station of claim 4, further comprising:

a reference signal transmitter satellite comprising a transmitter that transmits the reference signal; and

wherein the receiver of the at least one of the satellite module is configured to wirelessly receive the reference signal from transmitter on the reference signal transmitter satellite.

7. The space-based solar power station of claim 4, wherein the receiver to wirelessly receive the reference signal comprises an amplifier, and a cleanup phase locked loop.

8. The space-based solar power station of claim 4, wherein each of the at least one satellite module also includes transmission lines that route the reference signal to at least one power transmitter on a given satellite module.

9. The space-based solar power station of claim 3, wherein the control electronics determine a phase shift to apply with respect to a received reference signal based upon location information.

10. The space-based solar power station of claim 1, wherein the at least one signal from the at least one sun sensor comprises signals corresponding to the sensor'"'"'s relative angle with respect to the sun.

11. The space-based solar power station of claim 10, further comprising at least one accelerometer disposed on the satellite module that is in signal communication with the microcontroller.

12. The space-based solar power station of claim 10, further comprising at least one gyroscope disposed on the satellite module that is in signal communication with the microcontroller.

13. The space-based solar power station of claim 10, wherein the microcontroller is configured to integrate the at least one sun sensor signals to generate a finite model of the power generation tile.

14. The space-based solar power station of claim 13, wherein the integration of the at least one sun sensor signals includes applying a Kalman filter to the at least one sun sensor signals.

15. The space-based solar power station of claim 13, wherein the integration of the at least one sun sensor signals includes applying an extended Kalman filter to the at least one sun sensor signals.

16. The space-based solar power station of claim 13, wherein the microcontroller is further configured to estimate the shape of the power generation tile with respect to the sun.

17. The space-based solar power station of claim 13, wherein the microcontroller is further configured to estimate the relative position of the antennas in the power transmitters with respect to each other.

18. The space-based solar power station of claim 17, wherein the microcontroller is further configured to communicate a signal to the control electronics to adjust the reference signal based upon the estimated relative positions of the antennas in the power transmitters with respect to each other.

19. The space-based solar power station of claim 1, wherein the control electronics is contained within an integrated circuit comprising:

an RF synthesizer configured to generate an RF signal based upon a received reference signal;

a phase adjuster configured to phase shift an RF signal received from the RF synthesizer by an amount determined by a control signal;

a power amplifier configured to amplify a phase shifted RF signal received from the phase adjuster; and

a digital signal processor configured by software stored in memory to generate the control signal for the phase adjuster.