Systems and applications of lighter-than-air (LTA) platforms
원문보기
IPC분류정보
국가/구분
United States(US) Patent
등록
국제특허분류(IPC7판)
G05D-001/00
G01S-019/13
B64B-001/46
B64B-001/62
B65B-001/44
G07C-005/08
출원번호
US-0434036
(2017-02-15)
등록번호
US-9658618
(2017-05-23)
발명자
/ 주소
Knoblach, Gerald M.
Frische, Eric A.
Barkley, Bruce Alan
출원인 / 주소
SPACE DATA CORPORATION
대리인 / 주소
Pillsbury Winthrop Shaw Pittman LLP
인용정보
피인용 횟수 :
2인용 특허 :
172
초록▼
Innovative new systems and method of operating the systems, wherein the system comprises an airborne platform comprising an unmanned balloon; a payload that is separate from the unmanned balloon; a transceiver; a flight termination device; at least two separate power sources; a sensor; a processor;
Innovative new systems and method of operating the systems, wherein the system comprises an airborne platform comprising an unmanned balloon; a payload that is separate from the unmanned balloon; a transceiver; a flight termination device; at least two separate power sources; a sensor; a processor; a pump; a valve; and an object that when broken separates the unmanned balloon and the payload, are disclosed herein.
대표청구항▼
1. A system comprising a plurality of airborne platforms, each airborne platform comprising an unmanned balloon; a payload that is separate from the unmanned balloon; a transceiver; a flight termination device; at least two separate power sources for the flight termination device; a sensor; a proces
1. A system comprising a plurality of airborne platforms, each airborne platform comprising an unmanned balloon; a payload that is separate from the unmanned balloon; a transceiver; a flight termination device; at least two separate power sources for the flight termination device; a sensor; a processor; a pump; and a valve; wherein the pump and the valve are configured to change an altitude of the airborne platform;wherein the sensor comprises a pressure sensor;wherein, in operation, the unmanned balloon substantially drifts along with the wind currents;wherein the transceiver is capable of communicating with a communication device that is separate from the unmanned balloon;wherein the flight termination device has an ability to terminate a flight of the unmanned balloon;wherein at least one of the geographical coordinates tracking system comprises a GPS;wherein the unmanned balloon is configured to operate above an attitude of about 60,000 feet;wherein the unmanned balloon has a flight duration capability that is longer than that of weather balloons that have flight durations of approximately 2 hours;wherein the payload is configured to communicate with an additional airborne payload attached to a separate unmanned balloon. 2. The system of claim 1, the system further comprising an antenna and at least two geographical coordinates tracking system. 3. The system of claim 1, wherein the payload remains attached to the unmanned balloon as one when landed unless the payload is separated from the unmanned balloon. 4. The system of claim 1, wherein the unmanned balloon substantially drifts along with the wind currents taking into account the wind currents. 5. The system of claim 1, wherein the unmanned balloon substantially drifts along with the wind currents taking into account the wind currents to prevent the airborne platform from becoming an uncontrolled lighter-than-air airborne platform. 6. A system comprising a plurality of airborne platforms, each airborne platform comprising an unmanned balloon; a payload that is separate from the unmanned balloon; a transceiver; a flight termination device; at least two separate power sources; a sensor; a processor; a pump; and a valve; and an object that when broken separates the unmanned balloon and the payload; wherein the pump and the valve are configured to change an altitude of the airborne platform;wherein the flight termination device has an ability to terminate a flight of the unmanned balloon;wherein at least one of the geographical coordinates tracking system comprises a GPS;wherein the unmanned balloon is configured to operate above an attitude of about 60,000 feet;wherein the unmanned balloon has a flight duration capability that is longer than that of weather balloons that have flight durations of approximately 2 hours;wherein the flight termination device has an ability to terminate a flight of the unmanned balloon based on a determination that further operation of the unmanned balloon presents a danger to air traffic; andwherein the flight termination device has an ability to terminate a flight of the unmanned balloon based on a determination of a malfunction of the unmanned balloon. 7. The system of claim 6, the system further comprising an antenna and at least two geographical coordinates tracking system wherein the sensor comprises a pressure sensor; wherein the at least two separate power sources are for powering the flight termination device; wherein, in operation, the unmanned balloon substantially drifts along with the wind currents; wherein the payload remains attached to the unmanned balloon as one when landed unless the payload is separated from the unmanned balloon; wherein the transceiver is capable of communicating with a communication device that is separate from the unmanned balloon. 8. The system of claim 6, wherein the airborne platform is configured to reduce or eliminate a chance of the airborne platform becoming a free floating, uncontrolled transmitter. 9. The system of claim 8, wherein the airborne platform is configured to reduce or eliminate a chance of the airborne platform becoming a free floating, uncontrolled transmitter by monitoring sensed information of the airborne platform and by comparing the sensed information to known geographic or altitude based boundaries. 10. The system of claim 9, wherein the sensed information comprises coordinates and velocities. 11. The system of claim 6, wherein the object comprises a line. 12. The system of claim 6, wherein the payload is configured to communicate with an additional airborne payload attached to a separate unmanned balloon. 13. The system of claim 6, wherein the unmanned balloon substantially drifts along with the wind currents taking into account the wind currents. 14. The system of claim 6, wherein the unmanned balloon substantially drifts along with the wind currents taking into account the wind currents to prevent the airborne platform from becoming an uncontrolled lighter-than-air airborne platform. 15. A method comprising operating a system, the system comprising: a plurality of airborne platforms, each airborne platform comprising an unmanned balloon; a payload that is separate from the unmanned balloon; a transceiver; a flight termination device; at least two separate power sources for the flight termination device; a sensor; a processor; a pump; and a valve;wherein the pump and the valve are configured to change an altitude of the airborne platform;wherein the sensor comprises a pressure sensor;wherein, in operation, the unmanned balloon substantially drifts along with the wind currents;wherein the transceiver is capable of communicating with a communication device that is separate from the unmanned balloon;wherein the flight termination device has an ability to terminate a flight of the unmanned balloon;wherein at least one of the geographical coordinates tracking system comprises a GPS;wherein the unmanned balloon is configured to operate above an attitude of about 60,000 feet;wherein the unmanned balloon has a flight duration capability that is longer than that of weather balloons that have flight durations of approximately 2 hours;wherein the payload is configured to communicate with an additional airborne payload attached to a separate unmanned balloon; andtransmitting data from the airborne platform. 16. The method of claim 15, the system further comprising an antenna and at least two geographical coordinates tracking system. 17. The method of claim 15, wherein the payload remains attached to the unmanned balloon as one when landed unless the payload is separated from the unmanned balloon. 18. The method of claim 15, wherein the unmanned balloon substantially drifts along with the wind currents taking into account the wind currents. 19. The method of claim 15, wherein the unmanned balloon substantially drifts along with the wind currents taking into account the wind currents to prevent the airborne platform from becoming an uncontrolled lighter-than-air airborne platform. 20. A method comprising operating a system, the system comprising: a plurality of airborne platforms, each airborne platform comprising an unmanned balloon; a payload that is separate from the unmanned balloon; a transceiver; a flight termination device; at least two separate power sources; a sensor; a processor; a pump; and a valve; and an object that when broken separates the unmanned balloon and the payload;wherein the pump and the valve are configured to change an altitude of the airborne platform;wherein the flight termination device has an ability to terminate a flight of the unmanned balloon;wherein at least one of the geographical coordinates tracking system comprises a GPS;wherein the unmanned balloon is configured to operate above an attitude of about 60,000 feet;wherein the unmanned balloon has a flight duration capability that is longer than that of weather balloons that have flight durations of approximately 2 hours;wherein the flight termination device has an ability to terminate a flight of the unmanned balloon based on a determination that further operation of the unmanned balloon presents a danger to air traffic; andwherein the flight termination device has an ability to terminate a flight of the unmanned balloon based on a determination of a malfunction of the unmanned balloon; andtransmitting data from the airborne platform. 21. The method of claim 20, the system further comprising an antenna and at least two geographical coordinates tracking system wherein the sensor comprises a pressure sensor; wherein the at least two separate power sources are for powering the flight termination device; wherein, in operation, the unmanned balloon substantially drifts along with the wind currents; wherein the payload remains attached to the unmanned balloon as one when landed unless the payload is separated from the unmanned balloon; wherein the transceiver is capable of communicating with a communication device that is separate from the unmanned balloon. 22. The method of claim 20, wherein the airborne platform is configured to reduce or eliminate a chance of the airborne platform becoming a free floating, uncontrolled transmitter. 23. The method of claim 22, wherein the airborne platform is configured to reduce or eliminate a chance of the airborne platform becoming a free floating, uncontrolled transmitter by monitoring sensed information of the airborne platform and by comparing the sensed information to known geographic or altitude based boundaries. 24. The method of claim 23, wherein the sensed information comprises coordinates and velocities. 25. The method of claim 20, wherein the object comprises a line. 26. The method of claim 20, wherein the payload is configured to communicate with an additional airborne payload attached to a separate unmanned balloon. 27. The method of claim 20, wherein the unmanned balloon substantially drifts along with the wind currents taking into account the wind currents. 28. The method of claim 20, wherein the unmanned balloon substantially drifts along with the wind currents taking into account the wind currents to prevent the airborne platform from becoming an uncontrolled lighter-than-air airborne platform.
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