Satellite capturing/tracking method and apparatus capable of reducing workloads of earth station

• US 6,061,019 A
• Filed: 07/01/1998
• Issued: 05/09/2000
• Est. Priority Date: 07/01/1997
• Status: Expired due to Fees

• Current Assignee: NEC Corporation
• Original Assignee: NEC Corporation
• Inventors: Miyoshi, Hiroaki
• Primary Examiner(s): Issing, Gregory C.
• Application Number:
  US09/108,821
• Time in Patent Office: 678 Days
• Field of Search: 342/359, 342/352, 342/430, 342/354, 342/356, 342/353, 342/357.09, 455/427, 455/430, 455/12.1
• US Class Current: 342/359
• CPC Class Codes: B64G 1/1007 Communications satellites
• CPC Class Codes: B64G 3/00 Observing or tracking cosmonautic vehicles

Abstract

A satellite capturing/tracking apparatus including: an antenna drive unit for driving an antenna in such a manner that said antenna is directed to a direction along which electromagnetic waves are transmitted from either a data relay satellite or a space station in response to a capturing/tracking command; an orbit/position detecting unit for receiving clock signals transmitted from a plurality of GPS satellites to calculate and output the present orbit and position of said apparatus as orbit/position information; a first storage unit for previously storing therein a capturing/tracking sequence program with relative time instants, produced by an azimuth angle and an elevation angle of either said data relay satellite or said space station; a second storage unit for storing therein data used to define a relationship between said azimuth angle, said elevation angle, and the orbit/position of said apparatus with respect to either said data relay satellite or said space station; and a capturing/tracking control unit for producing a capturing/tracking command for capturing/tracking either said data relay satellite or said space station based on said orbit/position information of said orbit/position detecting unit, said capturing/tracking sequence program of said first storage unit, and said relationship data of said second storage unit; whereby, while data is communicated via said data relay satellite between the space station and an earth station, said space station and the data relay satellite are mutually captured/tracked with each other.

Claims

1. A satellite capturing/tracking apparatus for use with an earth station disposed on the surface of the earth, a space station in orbit around the earth for communicating data with said earth station, and a data relay satellite in orbit around the earth station for relaying said data between said space station and said earth station, wherein one of said data relay satellite or said space station contains the apparatus, the apparatus comprising:

an antenna drive unit for driving an antenna in such a manner that said antenna is directed to a direction along which electromagnetic waves are transmitted from the other of said data relay satellite or said space station in response to a capturing/tracking command;

an orbit/position detecting unit for receiving clock signals transmitted from a plurality of GPS satellites to calculate and output a present orbit and position of said one of said data relay satellite or said space station containing the apparatus as orbit/position information;

a first storage unit for previously storing therein a capturing/tracking sequence program with relative time instants, consisting of an azimuth angle and an elevation angle of the other of said data relay satellite or said space station;

a second storage unit for storing therein data used to define a relationship between said azimuth angle, said elevation angle, and the orbit/position of said one of said data relay satellite or said space station containing the apparatus with respect to the other of said data relay satellite or said space station; and

a capturing/tracking control unit for producing a capturing/tracking command for capturing/tracking the other of said data relay satellite or said space station based on said orbit/position information of said orbit/position detecting unit, said capturing/tracking sequence program of said first storage unit, and said relationship data of said second storage unit;

whereby, while said data is communicated via said data relay satellite between said space station and said earth station, said space station and said data relay satellite are captured/tracked with each other without the assistance of said earth station.

2. A satellite capturing/tracking apparatus according to claim 1, wherein said orbit/position information corresponds to an orbit element of said one of said data relay satellite or said space station containing the apparatus and longitude/latitude of an orbit plane projected on the earth surface;

and

said relationship data stored in said second storage unit corresponds to visible/invisible information about the other of said data relay satellite or said space station with respect to the longitude/latitude of said one of the data relay satellite or said space station containing the apparatus.

3. A satellite capturing/tracking apparatus according to claim 1, wherein said first storage unit and said second storage unit are constituted by data rewritable memories.

4. A satellite capturing/tracking according to claim 1, wherein said capturing/tracking command supplied to said antenna drive unit contains drive angle/drive velocity, and said antenna drive unit produces an angle signal of said antenna.

5. A satellite capturing/tracking method in which an earth station is disposed on the surface of the earth, a space station is in orbit around the earth for communicating data with said earth station, and a data relay satellite is in orbit around the earth station for relaying said data between said space station and said earth station, wherein the method comprising the steps of:

driving an antenna at one of said data relay satellite or space station in such a manner that said antenna is directed to a direction along which electromagnetic waves are transmitted from the other of said data relay satellite or said space station in response to a capturing/tracking command;

receiving clock signals at said one of said data relay satellite or space station transmitted from a plurality of GPS satellites to calculate and output a present orbit and position of said one of said data relay satellite or space station as orbit/position information;

previously storing at said one of said data relay satellite or space station in a first storage unit thereof, a capturing/tracking sequence program with relative time instants, consisting of an azimuth angle and an elevation angle of the other of said data relay satellite and said space station;

storing at said one of said data relay satellite or space station in a second storage unit thereof, data used to define a relationship between said azimuth angle, said elevation angle, and said orbit/position of said one of said data relay satellite or space station with respect to the other of said data relay satellite or said space station; and

producing at said one of said data relay satellite or space station a capturing/tracking command to capture/track the other of said data relay satellite or said space station based on said orbit/position information, said capturing/tracking sequence program, and said relationship data;

whereby, while said data is communicated via said data relay satellite between said space station and said earth station, said space station and said data relay satellite are captured/tracked with each other without the assistance of said earth station.

6. A satellite capturing/tracking method according to claim 5, wherein said orbit/position information corresponds to an orbit element of said one of said data relay satellite or space station and longitude/latitude of an orbit plane projected on the earth surface;

and

said relationship data corresponds to visible/invisible information about the other of said data relay satellite or said space station with respect to the longitude/latitude of said one of said data relay satellite or space station.

7. A satellite method according to claim 5, wherein said capturing/tracking command supplied in said antenna driving step contains drive angle/drive velocity, and at said antenna driving step, an angle signal of said antenna is produced.