IP Library Granted Patent US 11,968,029
Granted Patent B2
US 11,968,029 · App. 17/421,795 · Granted Apr 23, 2024

Device and a method for transmitting communications in a satellite network using beam-hopping

Inventors: Doron Rainish (Ramat Gan, IL); Avraham Freedman (Tel Aviv, IL)
Assignee: SATIXFY ISRAEL LTD.
H04B7/18515H04L27/2602H04W16/28H04W84/06
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Quick Facts
Patent No.
US 11,968,029
App. No.
17/421,795
Granted
Apr 23, 2024
Kind
B2
Abstract

A transceiver is provided which is configured to be used in a satellite communications network and adapted to superframes having variable lengths, wherein at least one of the received superframes has standard payload capacity units (P) and known symbols (D).

Claims (77)

1. A method for use in a satellite communications network, comprising:

transmitting and/or receiving superframes according to a pre-scheduled beam hopping time plan having different dwell times of cells of a plurality of cells within said satellite communications network,

which superframes comprise payload capacity units and dummy symbols and have variable lengths, as defined by a number of payload capacity units (P) in a superframe,

wherein the method comprises

determining:

said number of payload capacity units (P) according to a dwell time for transmission of said superframe and according to a beam switching time;

a number of dummy symbols (D), according to said beam switching time by multiplying said beam switching time by said symbol rate, according to the following relationship equation:

D =(said dwell time)*(said symbol rate)−(said header length)−(said capacity unit size)*said number of payload units ( P ).

2. The method according to claim 1 , wherein said determining is according to a symbol rate.

3. The method according to claim 1 , comprising receiving a multi-carrier signal having different symbol rates per carrier;

wherein said determining, for each carrier, comprises determining said payload capacity units (P) according to a symbol rate of said carrier.

4. The method according to claim 1 , wherein said determining comprises determining said number of payload capacity units (P), according to the following relationship:

P =[((said dwell time-said beam switching time)*(said symbol rate)−a header length)/(a capacity unit size)].

5. The method according to claim 1 , wherein said transmitting comprises embedding regular DVB-S2/S2X frames within said superframe.

6. The method according to claim 1 , wherein said transmitting comprises splitting a regular frame between two or more of said superframes.

7. The method according to claim 1 , wherein said dummy symbols comprise a dummy symbol header.

8. The method according to claim 7 , wherein said dummy symbol header is as defined in the DVB-S2X Annex E, format 4, 5, 6, or 7 Communication Standard.

9. The method according to claim 7 , wherein said transmitting is by a transmitter;

wherein said method comprises turning off said transmitter once said dummy symbol header has been transmitted.

10. The method according to claim 1 , comprising receiving said superframe,

wherein said receiving comprises identifying an end of said superframe by recognizing a dummy frame header.

11. The method according to claim 1 , further comprising a step of beam hopping, wherein said receiving is by a receiver of said satellite communications network, wherein said dwell time is not known in advance to said receiver.

12. The method according to claim 1 , wherein said superframe comprises a synchronization preamble, followed by a said payload capacity units and ending with a postamble.

13. The method according to claim 12 , wherein said synchronization preamble includes a SOH header, and wherein said postamble is an EOH postamble.

14. The method according to claim 12 , wherein said payload capacity units are in a form of DVB-S2X PLFRAMEs wherein said determining comprises determining a number and type of PLFRAMES according to communications traffic being conveyed, and according to types of terminals located within an illuminated cell of said plurality of cells.

15. A transceiver for a satellite communications network having a plurality of cells employing a pre-scheduled beam hopping time plan having different dwell times for cells of the plurality of cells, which transceiver is configured to:

transmit and/or receive superframes comprising payload capacity units and dummy symbols and having variable lengths, by determining:

a number of payload capacity units (P) in a superframe, according to a dwell time for transmission of said superframe and according to a beam switching time;

a number of dummy symbols (D), according to said beam switching time by multiplying said beam switching time by said symbol rate, according to the following relationship equation:

D =(said dwell time)*(said symbol rate)−(said header length)−(said capacity unit size)*said number of payload units ( P ).

16. The transceiver according to claim 15 , wherein said determining is according to a symbol rate.

17. The transceiver according to claim 15 , wherein said transceiver is configured to receive a multi-carrier signal having different symbol rates per carrier;

wherein said determining, for each carrier, comprises determining said payload capacity units (P) according to a symbol rate of said carrier.

18. The transceiver according to claim 15 , wherein said determining comprises determining said number of payload capacity units (P), according to the following relationship:

P

=

(

said

dwell

time

-

said

beam

switching

time

)

*

(

said

symbol

rate

)

-

a

header

length

a

capacity

unit

size

.

19. The transceiver according to claim 15 , wherein said transceiver is configured embed regular DVB-S2/S2X frames within said superframe.

20. The transceiver according to claim 15 , wherein said transceiver is configured to transmit superframes by splitting a regular frame between two or more of said superframes.

Assignments (5)
RELEASE OF SECURITY INTEREST IN PATENT COLLATERAL Recorded Mar 6, 2026
From: MDA SPACE LTD. (FORMERLY MDA LTD.)
To: MDA SPACE ISREAL LTD. (FORMERLY SATIXFY ISRAEL LIMITED)
Reel/Frame 075020/0743 →
RELEASE OF SECURITY INTEREST Recorded Jul 8, 2025
From: WILMINGTON SAVINGS FUND SOCIETY, FSB
To: SATIXFY ISRAEL LTD; SATIXFY UK LIMITED
Reel/Frame 071624/0152 →
SECURITY INTEREST Recorded Oct 31, 2023
From: SATIXFY ISRAEL LTD; SATIXFY UK LIMITED
To: MDA LTD.
Reel/Frame 065409/0382 →
FIRST SUPPLEMENT TO GRANT OF SECURITY INTEREST IN PATENT RIGHTS Recorded Oct 30, 2023
From: SATIXFY ISRAEL LTD
To: WILMINGTON SAVINGS FUND SOCIETY, FSB, AS ADMINSTRATIVE AGENT
Reel/Frame 065393/0808 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Sep 6, 2022
From: RAINISH, DORON; FREEDMAN, AVRAHAM
To: SATIXFY ISRAEL LTD.
Reel/Frame 061000/0033 →
Continuity (2)
Provisional Application 62790506 · Jan 10, 2019
Related Publication 20220094428A1 · Mar 24, 2022