Radio frequency sharing methods for satellite systems

• US 5,926,758 A
• Filed: 08/26/1996
• Issued: 07/20/1999
• Est. Priority Date: 08/26/1996
• Status: Expired due to Fees

• Current Assignee: Leo One IP, LLC
• Original Assignee: Leo One IP, LLC
• Inventors: Marshall, James M., Grybos, David P.
• Primary Examiner(s): LE, THANH C
• Application Number:
  US08/703,228
• Time in Patent Office: 1,058 Days
• Field of Search: 455/427, 455/429, 455/430, 455/447, 455/454, 455/12.1, 455/13.1, 455/62, 455/63, 455/428
• US Class Current: 455/429
• CPC Class Codes: H04B 7/18513 Transmission in a satellite or space-based system
• CPC Class Codes: H04B 7/195 Non-synchronous stations
• CPC Class Codes: Y02D 30/70 in wireless communication networks

Abstract

Methods and apparatus are disclosed which allow many satellites (A1-M, B1-N) in a plurality of Systems (A, B) to use the same radio frequencies (f1-n) so long as there is no interference between radio signals. The methods compute times (t) when satellite radio signals (32, 36) have overlapping reception areas or "footprints" (30, 35) on the Earth'"'"'s surface (E) whereby a user'"'"'s reception or transmission of a message would be interfered unless different frequencies (f1-n) are used for the "competing" signals. The methods use a timing algorithm that does not allow two satellites (Ai, Bi) which are "visible" at the same point on the Earth (E) to transmit on the same frequency (fi). In one preferred embodiment, a timing algorithm (48) produces a radio frequency use schedule (49) computed on the Earth from orbital data maintained in an ephemeris (46) of satellite communications systems (A, B) which communicate on frequencies (f1-n) giving rise to interfering radio signals. The radio frequency use schedule (49) is updated frequently, and is transmitted to and stored on board each satellite in System A (A1-M). System A satellites (A1-M) are then operated in accordance with the radio frequency use schedule (49).

Claims

1. A method of radio frequency sharing between satellites (A1-M) in a first System (A) and satellites (B1-N) in a second System (B), said satellites of said first System (A) being in communication with Earth (E) through a plurality of ground relay stations (18) and user terminals (20), said first System (A) having a plurality of orbit planes (14, 15) containing said satellites (A1-M), the method comprising the steps of:

assigning an initial communication frequency to all said satellites (A1-M) in each one of said plurality of orbit planes (14,

     15) of said first System (A);

said initial communication frequency being identical for all satellites (A1-M) residing in a same orbital plane (14,

     15);

changing said initial communication frequency (f_Ai) assigned to one of said satellites (Ai) residing in a first one of said orbital planes (14) of said first System (A), to a frequency (f_Aj) assigned to satellites (Aj) residing in a second one of said orbital planes (15) of said first System (A), when a radio beam footprint (30) of said satellite (Ai) overlaps a radio beam footprint (35) of one of said satellites (B1-N ) residing in said second System (B) and said radio frequencies being in use by respective said satellites (A1-M, B1-N) will interfere;

said frequency (f_Aj) being one which does not interfere with any other satellite (A1-M) in said first System (A) or a satellite (B1-N) in said second System (B), and

effecting timing of said changing said initial communication frequency (f_Ai) by using a radio frequency use schedule (49) computed in advance from orbital parameter ephemeris data (46) for said satellites (A1-M) in said first System (A) and satellites (B1-N) in said second System (B).

2. The method as claimed in claim 1, in which the step of changing said initial communication frequency (f_Ai) assigned to one of said satellites (Ai) residing in a first one of said orbital planes (14) of said first System (A), includes the step of changing said initial communication frequency (f_Ai) to a frequency (f_Aj) initially assigned to satellites (Aj) residing in orbit planes (14, 15) in which said satellites (Aj) do not present radio interference with satellites (A1-M) in other said planes (14, 15).

3. The method as claimed in claim 1, in which the step of assigning an initial communication frequency to all said satellites (A1-M) in each one of said plurality of orbit planes (14, 15) of said first System (A) further includes the step of:

assigning said initial communication frequency (f_Ai) by interleaving the frequency assignments to each of the orbital planes (14,

     15) of said first System (A) such that every odd numbered orbit plane is assigned a frequency from a first half of an authorized frequency spectrum and every even numbered orbit plane is assigned a frequency from a second half of the spectrum.

4. The method as claimed in claim 3, in which the step of assigning said initial communication frequency (f_Ai) by interleaving the frequency assignments to each of the orbital planes (14, 15) of said first System (A) includes the step of:

assigning said frequency from said first half of an authorized frequency spectrum in an order proceeding from a lower frequency (f1) to a higher frequency (f7) and assigning said frequency from said second half of an authorized frequency spectrum in an order proceeding from a higher frequency (f6) to a lower frequency (f2).

5. The method as claimed in claim 3, in which the step of changing said initial communication frequency (f_Ai) assigned to one of said satellites (Ai) residing in a first one of said orbital planes (14) of said first System (A), includes the step of changing said initial communication frequency (f_Ai) to a frequency (f_Aj) initially assigned to satellites (Aj) residing in an orthogonal orbit plane (15) of said first System (A).

6. The method as claimed in claim 5, in which said orthogonal orbit plane (15) is an inclined, orthogonal, conjugate orbit plane (15).

7. The method as claimed in claim 1, further including the step of

using packet transmission store and forward protocols for said communication between said satellites of said first System (A);

said plurality of ground relay stations (18) and said user terminals (20) to reduce infrequent interference between satellites in said first System (A) and said second System (B) caused by burst packet transmissions and packet re-transmissions.

8. The method as claimed in claim 3, in which the step of changing said initial communication frequency (f_Ai) assigned to one of said satellites (Ai) residing in a first one of said orbital planes (14) of said first System (A), includes the step of changing said initial communication frequency (f_Ai) to a frequency (fci) initially assigned to satellites (Ci) residing in a third System (C) in which said satellites (Ci) do not present radio interference with satellites (A1-M) in said first System (A).

9. The method as claimed in claim 1, in which the step of effecting timing of said changing said initial communication frequency (f_Ai) by using a radio-frequency use schedule (49) computed in advance from orbital ephemeris data (46) for said satellites (A1-M) in said first System (A) and satellites (B1-N) in said second System (B) includes the steps of:

listening for transmissions of satellites (B1-N) residing in said second System (B) with satellites (A1-M) residing in said first System (A);

intercepting said transmissions and determining the frequency (f_Bp) of said transmissions and time to change said initial communication frequency (f_Ai);

transmitting said frequency (f_Bp) and said time determined by said satellites (A1-M) to all said satellites (A1-M) in said first System (A) and to at least one of said plurality of ground relay stations (18); and

maintaining said frequency (f_Bp) and time as data in said orbital parameter ephemeris (46) and computing on board each of said satellites (A1-M) said radio frequency use schedule (49) by use of a radio frequency use schedule algorithm (48).

10. The method as claimed in claim 9, in which the step of maintaining said frequency (f_Bp) and time as data in said orbital parameter ephemeris (46) and computing said radio frequency use schedule (49), is accomplished on board each said satellite (A1-M).

11. The method as claimed in claim 9, in which the step of maintaining said frequency (f_Bp) and time as data in said orbital parameter ephemeris (46) and computing said radio frequency use schedule (49), is accomplished on the Earth (E) and furnished to each said satellite (A1-M) from one of said plurality of ground relay stations (18).