High-yield active printed-circuit antenna system for frequency-hopping space radar

• US 5,206,655 A
• Filed: 03/06/1991
• Issued: 04/27/1993
• Est. Priority Date: 03/09/1990
• Status: Expired due to Term

• Current Assignee: Alcatel Espace
• Original Assignee: Alcatel Espace
• Inventors: Cazaux, Jean-Louis, Caille, Gerard, Remondiere, Olivier
• Primary Examiner(s): Hille, Rolf
• Assistant Examiner(s): BROWN, PETER T
• Application Number:
  US07/665,212
• Time in Patent Office: 783 Days
• Field of Search: 342/25, 342/361, 342/368, 343/700 MS File, 343/853, 343/701
• US Class Current: 343/700.0MS
• CPC Class Codes: G01S 7/032 Constructional details for solid-state radar subsystems
• CPC Class Codes: H01Q 21/0025 Modular arrays
• CPC Class Codes: H01Q 21/245 provided with means for varying the polarisation polarising devices H01Q15/24; tracking by comparing linear polarisation compounds G01S3/146; reducing depolarisation effects H04B7/00; polarisation diversity H04B7/10
• CPC Class Codes: H01Q 3/26 varying the relative phase or relative amplitude of energisation between two or more active radiating elements; varying the distribution of energy across a radiating aperture H01Q3/12, H01Q3/22, H01Q3/24 take precedence

Abstract

A high-efficiency active printed-circuit antenna system for pulsed frequency-hopping space radar electronically scanned in two planes encompasses in its timing diagram the transmission of a horizontal polarization pulse, the reception of echoes from a previous horizontal polarization pulse, the transmission of a vertical polarization pulse and the reception of echoes from a previous vertical polarization pulse. The system comprises several thousand MMIC modules distributed over the antenna and each connected to a printed-circuit radiating element comprising a plurality of dual polarized square patches connected by microstrip lines which excite them with the same amplitude and the same phase at two perpendicular ports. Switching between the two ports procures transmission or reception with horizontal or vertical polarization.

Claims

1. High-yield antenna system including an active printed-circuit planar antenna for pulsed frequency-hopping space radar electronically scanned in two planes, its timing diagram encompassing the transmission of a horizontal polarization pulse, the reception of echoes from a previous horizontal polarization pulse, the transmission of a vertical polarization pulse and the reception of echoes from a previous vertical polarization pulse, said system comprising, distributed on insulative substrates, several thousand MMIC active transmit-receive modules, each of which contains a switching device, amplifier means and a phase shifter, and each of which is connected to one of a plurality of printed-circuit radiating elements, each printed-circuit radiating element comprising a plurality of dual polarized square patches connected by microstrip lines adapted selectively to excite the patches with the same amplitude and the same phase at two perpendicular ports coupled to said switching device, said switching device switching between said two ports for selectively procuring transmission or reception with horizontal or vertical polarization.

2. Antenna system according to claim 1 wherein each MMIC active module has an output power of 1 W or less.

3. Antenna system according to claim 1 wherein the active modules of said antenna system are subdivided into modular subarrays to be assembled together.

4. Antenna system according to claim 1, further comprising a plurality of redundant transmit-receive MMIC active modules each containing a switching device and amplifier means, and wherein identical integrated circuits are used in said redundant active modules and in said active modules which are disposed immediately behind the radiating elements.

5. Antenna system according to claim 1 wherein said switching device comprises a double-pole/double-throw switch implementing transmit/receive and horizontal/vertical polarization switching functions.

6. Antenna system according to claim 1 wherein the active modules are implemented in hybrid technology and comprise an output circulator.

7. Antenna system according to claim 1 further comprising primary and secondary mechanical structures for supporting the antenna comprising:

very lightweight materials suitable for spacecraft applications, such lightweight materials having sufficient structural stiffness to limit deformations of the antenna to less than 2 mm for a planar antenna larger than 8 m×

2 m; and

a thermo-elastically decoupled link system between said primary and secondary mechanical structures of the antenna system.

8. Antenna system according to claim 1 comprising multi-layer insulation at a rear and edges of the planar antenna, and a white-colored randome adapted to radiate heat in a forward direction away from the front surface of the planar antenna.

9. Antenna system according to claim 1 comprising a laser sighting system, mirrors distributed over the antenna, and a computer for correcting control signals applied to the phase shifters in the active modules for compensating for deformations of the antenna.

10. The antenna system according to claim 1 wherein the number of said MMIC modules is more than 6,000, wherein the number of said patches and said microstrip lines is more than 49,000, wherein said planar antenna has a surface area of 18.6 m², wherein each combination of a radiating element and an active module occupies an area of 1.88×

16 cm and wherein the antenna system has a weight equal to or less than 700 kg, so that said antenna system is compatible with space-environmental constraints such as weight, electrical energy consumption, radiation hardness, and ruggedness and robustness/reliability with respect to the module failures.