IP Library Granted Patent US 11,709,273
Granted Patent B2
US 11,709,273 · App. 16/204,968 · Granted Jul 25, 2023

Stratospheric position, navigation, and timing system

Inventors: Jared Ernest Kocer (Sioux Falls, SD); Scott William Wickersham (Brandon, SD); Bart Gallet (Arlington, VA)
G01S19/10G01S19/46G01S19/03G01S19/12
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Quick Facts
Patent No.
US 11,709,273
App. No.
16/204,968
Granted
Jul 25, 2023
Kind
B2
Abstract

Disclosed in some examples are methods, systems, devices, and machine-readable mediums for providing a PNT system provided by stratospheric balloons. This stratospheric PNT system (SPNTS) replaces the space-segment of a standard PNTS with a stratospheric segment comprising one or more stratospheric balloons that provide PNTS signals usable to determine timing, positioning, and/or navigation for user devices.

Claims (29)

1. A device comprising:

a balloon;

a computing device coupled to the balloon, the computing device comprising:

a hardware processor configured to:

determine a geolocation of the balloon;

create almanac data comprising locations of a plurality of other balloons based upon peer-to-peer messages exchanged with the plurality of other balloons; and

a transceiver configured to:

broadcast a signal based upon the geolocation that includes data useable by a user segment receiver for trilateration as part of resolving its global position, the signal a same format and frequency as signals sent by a Global Navigation Satellite System (GNSS), the signal including the almanac data.

2. The device of claim 1 , wherein the transceiver is further configured to broadcast a ranging code.

3. The device of claim 1 , wherein the hardware processor is configured to determine the geolocation of the balloon based upon geolocation signals received from a plurality of ground based reference signals.

4. The device of claim 1 , wherein the computing device coupled to the balloon includes a sensor, and wherein the hardware processor is configured to determine the geolocation of the balloon based upon an output of the sensor.

5. The device of claim 4 , wherein the sensor is an inertial measurement unit.

6. The device of claim 4 , wherein the sensor is a barometer.

7. The device of claim 4 , wherein the sensor is an optical sensor.

8. The device of claim 4 , wherein the sensor is one of: a directional RF sensor array, a magnetometer, RADAR, radio navigation aids.

9. The device of claim 4 , wherein the hardware processor is configured to determine the geolocation of the balloon by inputting the output of the sensor into a Bayesian filter to produce estimated geolocation coordinates.

10. The device of claim 4 , wherein the hardware processor is configured to determine the geolocation of the balloon from a message sent by a ground-based station and the output of the sensor.

11. The device of claim 1 , comprising an atomic clock.

12. The device of claim 11 , wherein the hardware processor is configured to synchronize the atomic clock to a plurality of atomic clocks in a plurality of other balloons.

13. A method of providing a signal for Positioning, Navigation, or Timing, the method comprising:

from a computing device coupled to a balloon, using a hardware processor to perform operations of:

determining a geolocation of the balloon;

creating almanac data comprising locations of a plurality of other balloons based upon peer-to-peer messages exchanged with the plurality of other balloons; and

broadcast a signal based upon the geolocation that includes data useable by a user segment receiver for trilateration as part of resolving its global position, the signal a same fomrn.t and frequency as signals sent by a Global Navigation Satellite System (GNSS), the signal including the almanac data.

14. The method of claim 13 , wherein the operations of determining the geolocation of the balloon comprises determining the geolocation of the balloon based upon geolocation signals received from a plurality of ground-based reference signals.

15. The method of claim 13 , wherein the operations of determining the geolocation of the balloon comprises determining the geolocation of the balloon based upon an output of a sensor that is both communicatively coupled to the hardware processor and attached to the balloon.

16. The method of claim 15 , wherein the sensor is one or more of: an inertial measurement unit, a barometer, an optical sensor, a celestial sensor, a directional RF sensor array, a magnetometer, radio detection and ranging (RADAR), and a radio navigational aid.

17. The method of claim 15 , wherein the operations of determining the geolocation of the balloon comprises determining the geolocation of the balloon by inputting the output of the sensor and a second sensor into a Bayesian filter to produce estimated geolocation coordinates.

18. The method of claim 15 , wherein the operations of determining the geolocation of the balloon comprise determining the geolocation of the balloon from a message sent by a ground-based station and the output of the sensor.

Assignments (3)
MERGER Recorded Oct 19, 2022
From: AEROSTAR INTERNATIONAL, INC.
To: AEROSTAR INTERNATIONAL, LLC
Reel/Frame 061727/0877 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Aug 22, 2022
From: RAVEN INDUSTRIES, INC.
To: AEROSTAR INTERNATIONAL, INC.
Reel/Frame 061297/0956 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Mar 19, 2019
From: KOCER, JARED ERNEST; WICKERSHAM, SCOTT WILLIAM; GALLET, BART
To: RAVEN INDUSTRIES, INC.
Reel/Frame 048638/0813 →
Continuity (2)
Provisional Application 62656845 · Apr 12, 2018
Related Publication 20190317220A1 · Oct 17, 2019
Cited By (1)
US 12,651,451