Dual-satellite emergency locator beacon and method for registering, programming and updating emergency locator beacon over the air
View Patent ↗A dual-satellite emergency locator beacon and method for programming and updating such emergency locator beacons over the air. The system uses a second commercial satellite as the carrier for the data back to the beacon together with the means of coupling these parts together. The system can be manually updated or can be part of a registration system that gets automatically updated. In a second embodiment a method and apparatus for implementing emergency locator beacon registration is provided. The system provides data concerning the user into a backend service which can be utilized to provide all necessary information needed to register the emergency beacon.
1. An emergency communications beacon, comprising:
a first satellite communications transmitter, a second satellite communications transmitter, a first microprocessor and a second microprocessor;
wherein said first microprocessor controls said first transmitter and said second microprocessor controls said second transmitter;
wherein said first transmitter is configured to communicate over a first satellite communications system and said second transmitter is configured to communicate over a second satellite communications system;
wherein said first and second microprocessors are interconnected to permit data transfer therebetween.
2. The beacon of claim 1 , wherein said second microprocessor is configured to receive data from said second satellite communications systems, over said second transmitter, and transfer said data to said first microprocessor.
3. The beacon of claim 1 , wherein said first microprocessor is configured to transmit and receive data from said second satellite communications systems by way of said second microprocessor.
4. The beacon of claim 3 , wherein said data comprises identity information of said first transmitter.
5. The beacon of claim 1 , wherein said first and second satellite communications systems are in bi-directional communication by way of an interface system; and wherein said first satellite communications system can transmit data to said beacon over said second satellite communications system by way of said interface system.
6. The system of claim 1 , wherein said first satellite communications system comprises a Cospas-Sarsat satellite system.
7. The system of claim 1 , wherein said second satellite communications system comprises a commercial satellite communications system.
8. The system of claim 7 , wherein said commercial satellite communications system comprises the Iridium satellite communications system.
9. The system of claim 1 , wherein said first transmitter comprises a Cospas-Sarsat transmitter and said second transmitter comprises Satellite Emergency Notification Device (SEND) transmitter.
10. The system of claim 1 , wherein said beacon further includes a global positioning receiver.
11. A method for programming an emergency communications beacon, comprising:
providing said emergency beacon, wherein said beacon includes a first satellite communications transmitter, a second satellite communications transmitter, a first microprocessor and a second microprocessor, wherein said first microprocessor controls said first transmitter and said second microprocessor controls said second transmitter;
establishing a communications link between said first transmitter and a first satellite communications system;
establishing a communications link between said second transmitter and a second satellite communications system;
establishing a data transfer link between said first microprocessor and said second microprocessor;
receiving on said second transmitter from said second satellite communications system, programming data;
processing said programming data from said second transmitter on said second microprocessor
transferring said programming data from said second microprocessor to said first microprocessor; and
processing said programming data on said first microprocessor to program said beacon.
12. The beacon of claim 11 , wherein said first microprocessor is configured to transmit and receive data from said second satellite communications systems by way of said second microprocessor.
13. The beacon of claim 12 , wherein said data comprises identity information of said first transmitter.
14. The beacon of claim 12 , wherein said first and second satellite communications systems are in bi-directional communication by way of an interface system; and wherein said first satellite communications system can transmit data to said beacon over said second satellite communications system by way of said interface system.
15. The system of claim 12 , wherein said first satellite communications system comprises a Cospas-Sarsat satellite system.
16. The system of claim 12 , wherein said second satellite communications system comprises a commercial satellite communications system.
17. The system of claim 16 , wherein said commercial satellite communications system comprises the Iridium satellite communications system.
18. The system of claim 12 , wherein said first transmitter comprises a Cospas-Sarsat transmitter and said second transmitter comprises Satellite Emergency Notification Device (SEND) transmitter.
19. The system of claim 12 , wherein said beacon further includes a global positioning receiver.