Granted Patent B2

US 7,406,311 · App. 11/543,916 · Granted Jul 29, 2008

Abstract

Claims (21)

1. A method for controlling first and second geosynchronous satellites in elliptical orbits in respective orbital planes in a satellite communication system, the satellite communication system providing at least one of a first frequency signal and a second frequency signal to receivers, the satellites each traversing a common ground track having a northern loop, a southern loop, and a crossover point between the northern and southern loops, the method comprising the steps of:

selecting said first frequency satellite signal to be transmitted from whichever of said first and second geosynchronous satellites is traversing said northern loop;

monitoring when said first and second geosynchronous satellites enter said northern loop and exit said northern loop;

switching via a satellite command system said first frequency signal to one of said first and second geosynchronous satellites when said satellite enters said northern loop;

powering down said first and second geosynchronous satellites when they are descending said southern loop below the equator; and

powering on said first and second geosynchronous satellites when they are ascending said southern loop from the equator.

2. A method as claimed in claim 1 , further comprising the step of transmitting said second frequency satellite signal from a third geosynchronous satellite.

3. A satellite command system for use in a satellite communication system comprising at least first and second geosynchronous satellites in elliptical orbits in two orbital planes in a time diversity system, the time diversity system providing both a first frequency signal and a second frequency signal to receivers, the elliptical orbit satellites each traversing a common ground track having a northern loop, a southern loop, and a crossover point between the northern and southern loops, the satellite communication system comprising a first uplink device for transmitting a first frequency satellite signal and a second uplink device for transmitting a second frequency satellite signal, the satellite command system comprising:

a device to determine and generate said data relating to the location of said elliptical orbit satellites along said common ground path; and

a processing device for monitoring when said elliptical orbit satellites enter said northern loop and exit said northern loop using said data and for generating commands depending on said data, said processing device being programmed to generate a command to operate said first uplink device to transmit said first frequency satellite signal to whichever one of said elliptical orbit satellites is traversing said northern loop.

4. A satellite command system as claimed in claim 3 , wherein satellite communication system comprises a third geosynchronous satellite, said processing device being programmed to generate a command to operate said second uplink device to transmit said second frequency satellite signal to said third geosynchronous satellite.

5. A satellite command system as claimed in claim 3 , wherein said processing device is programmed to a command to power down whichever one of said elliptical orbit satellites is traversing said southern loop below said equator.

6. A satellite command system as claimed in claim 3 , wherein said processing device is programmed to generate a command to operate said second uplink device to transmit said second frequency satellite signal to said satellite when said satellite exits said northern loop.

7. A satellite command system as claimed in claim 6 , wherein said processing device is programmed to generate a command to power down said satellite when said satellite descends said southern loop below the equator.

8. A satellite command system as claimed in claim 7 , wherein said processing device is programmed to generate a command to power on said satellite when said satellite ascends said southern loop from the equator.

9. A satellite command system as claimed in claim 8 , wherein said processing device is programmed to generate a command to operate said first uplink device to transmit said first frequency signal to said satellite when said satellite enters said northern loop.

10. A receiver in a time diversity system comprising first, second and third geosynchronous satellites in three elliptical orbits that are separated by approximately 120 degrees, the satellites each traversing a common ground track having a northern loop, a southern loop, and a crossover point between the northern and southern loops, the southern loop being intersected by the equator, the receiver comprising:

a receiving device for receiving a late satellite signal and an early satellite signal, said late satellite signal corresponding to said early satellite signal and delayed a selected period of time with respect to said early satellite signal, said late satellite signal and said early satellite signal being received from selected said satellites as they traverse said northern loop, said late satellite signal and said early satellite signal each comprising at least a portion of a broadcast stream having a plurality of program channels;

a memory buffer device connected to said receiving device and operable to store a subset of said plurality of program channels for a said selected period of time during reception of said early signal; and

a combining device connected to said receiving device and said memory buffer device for using at least one of said late satellite signal and an output signal from said memory buffer device to generate a program signal for playback via said receiver.

11. A receiver as claimed in claim 10 , further comprising a channel selecting device configured to receive said late satellite signal and said early satellite signal from said receiving device and to provide at least a portion of said broadcast stream to said memory buffer device in response to user selection of at least one of said plurality of program channels.

Assignments (8)