Distributed-array radar system comprising an array of interconnected elementary satellites

• US 4,843,397 A
• Filed: 03/25/1988
• Issued: 06/27/1989
• Est. Priority Date: 03/26/1987
• Status: Expired due to Fees

• Current Assignee: Finmeccanica SPA, Gaspare Galati
• Original Assignee: Gaspare Galati, Selenia Spazio S.p.A. (Leonardo S.p.A.)
• Inventors: Losquadro, Giacinto, Galati, Gaspare
• Primary Examiner(s): Tarcza, Thomas H.
• Assistant Examiner(s): Hellner, Mark
• Application Number:
  US07/173,727
• Time in Patent Office: 459 Days
• Field of Search: 342/59, 342/175, 342/352, 342/354, 342/368, 342/371, 342/372
• US Class Current: 342/59
• CPC Class Codes: B64G 1/1021 Earth observation satellites
• CPC Class Codes: B64G 1/1035 using radar for mapping, surveying or detection, e.g. of intelligence
• CPC Class Codes: B64G 1/1085 Swarms and constellations
• CPC Class Codes: B64G 3/00 Observing or tracking cosmonautic vehicles
• CPC Class Codes: G01S 13/42 Simultaneous measurement of distance and other co-ordinates indirect measurement G01S13/46
• CPC Class Codes: G01S 7/006 using shared front-end circuitry, e.g. antennas G01S13/765, G01S13/825 take precedence

Abstract

A radar system for primary and secondary airspace surveillance, and especially for the detection and tracking of moving targets, consisting of a number of elementary satellites connected to nonrigid structures and of a main satellite, which performs accurate measurement of the position and altitude of elementary satellites and real-time adaptive combination of radar signals coming from them, so as to provide a large-phased array operating in the microwave band. This system overcomes the limitations on dimensioned large space-bound antennae found in the literature, minimizing the incidence and effects of undesired echoes and interference and assuring high detection accuracy. The fact that the elementary satellites are all the same (modular) makes possible gradual assembly of the system with possible expansion in time and assures particularly high operating availability.

Claims

1. A radar system for primary and secondary surveillance of an airspace, comprising:

a plurality of elementary satellites spaced apart in a distributed array in space and each provided with;

an antenna element forming with the antenna elements of the other elementary satellites of the distributed array a phased array antenna of an area corresponding substantially to the area of said distributed array of elementary satellites,

receiver means connected to said antenna element for receiving radar signals from said airspace,

transmitter means connected to said antenna element for transmitting radar signals into said airspace, and

communication means for receiving signals for controlling the element and transmitting radar signals from the elementary satellite;

a main satellite spaced from said distributed array of elementary satellites in space and provided with communication means in communication with the communication means of each of said elementary satellites for transmitting signals for controlling the antenna element thereof and for receiving radar signals transmitted from individual ones of said elementary satellites; and

a ground station in wireless communication with said main satellite for receiving radar information from said main satellite corresponding to the radar signals received thereby and transmitted from the individual ones of said elementary satellites.

2. A radar system for primary and secondary surveillance of an airspace, comprising:

a plurality of elementary satellites spaced apart in a distributed array in space and each provided with;

an antenna element forming with the antenna elements of the other elementary satellites of the distributed array a phased array antenna of an area corresponding substantially to the area of said distributed array of elementary satellites,

receiver means connected to said antenna element for receiving radar signals from said airspace,

transmitter means connected to said antenna element for transmitting radar signals into said airspace, and

communication means for receiving signals for controlling the element and transmitting radar signals from the elementary satellite;

a main satellite spaced from said distributed array of elementary satellites in space and provided with communication means in communication with the communication means of each of said elementary satellites for transmitting signals for controlling the antenna element thereof and for receiving the transmitted radar signals from individual ones of said elementary satellites;

a ground station in wireless communication with said main satellite for receiving radar information from said main satellite corresponding to the radar signals received thereby and transmitted from the individual ones of said elementary satellites;

means interconnecting said elementary satellites in a generally planar array of polygonal outline to form a nonrigid structure with said elementary satellites;

a plurality of tension segments connected to said array and connected to said nonrigid structure to apply tension thereto;

a plurality of pulling satellites connected to said tension segments and exerting outward force on said nonrigid structure; and

dampers connected between satellites of said nonrigid structure for damping oscillation of the satellites of said nonrigid structure, said pulling satellites being provided with;

attitude and orbit control means for positioning said nonrigid structure in space, and

communication means connected to said attitude and orbit control means and receiving control signals from said main satellite for operating said attitude and orbit control means.

3. The radar system defined in claim 2, further comprising means connecting said main satellite to said nonrigid structure as an additional pulling satellite.

4. The radar system defined in claim 2 wherein said main satellite further comprises:

circuit means for combining the radar signals received from the individual ones of said elementary satellites coherently and adaptively so as to synthesize said phased array;

an antenna beamforming processor connected to said circuit means for generating an antenna beam pattern; and

a beamforming command generator connected to said antenna beamforming processor and to said communication means of said main satellite to attenuate sidelobes of said phased array and maximize a signal-to-noise ratio thereof.

5. The radar system defined in claim 2 wherein the antenna element of each of said elementary satellites is a phased-array antenna with coefficients determined on a basis of commands received from said main satellite and selected to attenuate sidelobes of the phased array and maximize a signal-to-noise ratio thereof.

6. The radar system defined in claim 4 wherein said main satellite further comprises:

a coder connected to said beamforming command generator for coding said coefficients;

a transmitter connected to said coder for transmitting coded coefficients to said elementary satellites; and

means forming an optical communications link forming part of said communication means of said main satellite and said elementary satellites and connected to the transmitter for transmitting coded coefficients to said elementary satellites.

7. The radar system defined in claim 2 wherein said main satellite further comprises:

a subsystem for accurately measuring positions of said pulling satellites and including a processor for generating orbit and attitude control commands for said pulling satellites;

a coder connected to said processor for coding said orbit and control commands for siid pulling satellites; and

a transmitter forming part of the communication means of said main satellite for transmitting coded orbit and attitude commands to said pulling satellites, said pulling satellites each being provided with;

ion motors responsive to the orbit and control means of the respective pulling satellite for driving the respective pulling satellite.

8. The radar system defined in claim 7 wherein said subsystem includes:

a laser telemeter;

an angle measurement unit for training said laser telemeter on said elementary and pulling satellites, said elementary and pulling satellites each having at least one laser retroreflector cooperating with said laser telemeter; and

a position computer connected to said angle measurement unit.

9. The radar system defined in claim 2 wherein each of said communication means includes:

a receiver on the respective satellite;

a decoder connected to said receiver for decoding signals received thereby;

a transmitter on the respective satellite; and

a coder connected to said transmitter for coding signals to be transmitted thereby.

10. The radar system defined in claim 2 wherein said main satellite further comprises:

receiver antenna means collecting radar signals from targets transmitted to said main satellite by said elementary satellites and combining said radar signals collected from said said targets, said communication means on said satellites including radiofrequency transmission links.

11. The radar system defined in claim 2 wherein the frequency of said transmission links is a multiple, submultiple or shifted frequency relative to the radar signal frequency emitted by said elementary satellites.

12. The radar system defined in claim 2 wherein said main satellite further includes:

a central computer connected to the communication means of said main satellite and storing data including;

ratio between sidelobes and peak of the phased array;

reflectivity of earth surface patterns within a range of a radiation patter of the phased array; and

geometry of radar resolution cells of interest, said central computer being provided with means for updating said data based upon information received from the ground.

13. The radar system defined in claim 2 wherein said main satellite further includes:

means for combining radar signals received from said elementary satellites with coefficients synthesizing a monopulse radiation pattern.

14. The radar system defined in claim 2 wherein said ground station includes:

a radar signal processor responsive to signals received from said main satellite; and

a radar signal extractor connected to said radar signal processor for determining positions of targets detected by said phased array.

15. The radar system defined in claim 2 wherein said main satellite further comprises:

means responsive to radar echoes from earth and SSR replies of transponders on earth at precisely known locations for continuously calibrating a position of said phased array and correcting beam pointing errors thereof and defocussing.

16. The radar system defined in claim 2 connected for defence and civil-aviation application.

17. The radar system defined in claim 2 at an altitude ranging from 1,000 km above the earth to a geostationary orbit altitude.

18. The radar system defined in claim 2 which comprises a plurality of said distributed arrays located in respective orbits for continuous surveillance of substantial portion of the globe to full global coverage.

19. The radar system defined in claim 18 wherein said main satellite communicates with a group of said distributed arrays for managing same.

20. The radar system defined in claim 18 wherein each of said distributed arrays is connected to a respective said main satellite for managing the respective distributed array.