Remote sensing apparatus for satellites

• US 4,748,448 A
• Filed: 06/28/1983
• Issued: 05/31/1988
• Est. Priority Date: 06/29/1982
• Status: Expired due to Fees

• Current Assignee: Agence Spatiale Europeenne
• Original Assignee: Agence Spatiale Europeenne
• Inventors: Thompson, Alan
• Primary Examiner(s): Tarcza, Thomas H.
• Assistant Examiner(s): Hellner, Mark
• Application Number:
  US06/508,541
• Time in Patent Office: 1,799 Days
• Field of Search: 343/5 W, 343/5 CM, 73/170 R, 342/25, 342/26, 342/82, 342/83, 342/85, 342/175, 342/352, 342/356
• US Class Current: 342/26.00A
• CPC Class Codes: G01S 13/42 Simultaneous measurement of distance and other co-ordinates indirect measurement G01S13/46
• CPC Class Codes: G01S 13/90 using synthetic aperture techniques , e.g. synthetic aperture radar [SAR] techniques
• CPC Class Codes: G01S 13/955 mounted on satellite
• CPC Class Codes: Y02A 90/10 Information and communication technologies [ICT] supporting adaptation to climate change, e.g. for weather forecasting or climate simulation

Abstract

The invention relates to remote sensing from a satellite of a parameter in one or more regions on the ground adjacent the satellite ground track by radar transmission. The purpose of the invention is to reduce energy consumption and optimize measurement accuracy. A transmitter antenna generates a plurality of pencil radar beams which illuminate respective cells of the region. A control means successively energizes the antenna at respective frequencies for respective pulse durations and for respective number of pulses. The invention is particularly appliable to scatterometer apparatus for responding to wind speed and direction by sensing radar backscatter from sea.

Claims

1. Remote sensing apparatus for use on board a satellite for sensing the differing values of a variable geophysical parameter in a plurality of measurement cells definable in at least one elongated region of the surface of the earth adjacent to the satellite ground track, said variable parameter altering the back-scatter coefficient of radar signal echos, said apparatus comprising:

transmitter-receiver means for illuminating said region with radar signals and receiving echos therefrom, said transmitter-receiver means including at least one frequency scanning antenna means, said transmitter-receiver means including control means for energizing said antenna means to transmit a succession of radar beams, each of said radar beams being transmitted at a predetermined angle of incidence to the earth'"'"'s surface and illuminating a cell in said region, each of said radar beams having a predetermined frequency and transmission power output selected in accordance with the transmission angle of incidence, said control means energizing said antenna means at substantially the same transmission power for time periods of differing lengths, thereby to control the transmission power output of said antenna means for each of said radar beams, and said transmitter-receiver means including signal processing means coupled to said antenna means for obtaining back-scatter coefficient properties of the radar signal echos and the values of the variable geophysical parameter.

2. Apparatus according to claim 1 wherein said antenna means illuminates a cell remote from the ground track at a large angle of incidence and illuminates at least one cell closer to the ground track at a small angle of incidence and wherein said control means is further defined as means for energizing said antenna means at substantially the same transmission power for time periods of greater length for said remote cell than for the closer cell, thereby to control the transmission power output and to obtain a substantially uniform measurement performance for each cell.

3. Apparatus according to claim 2 wherein said antenna means illuminates a cell remote from the ground track at a large angle of incidence and illuminates at least one cell closer to the ground track at a smaller angle of incidence and wherein said control means is further defined as means for energizing said antenna means at substantially the same transmission power with pulse trains having a greater number of pulses for said remote cell than for the closer cell.

4. Apparatus according to claim 2 wherein said control means is further defined as means for energizing said antenna means in a plurality of cycles, said antenna means being successively energized for differing portions of each of said cycles for controlling the transmitting time periods of said antenna means.

5. Apparatus according to claim 1 wherein said antenna means illuminates a cell remote from the ground track at a large angle of incidence and illuminates at least one cell closer to the ground track at a smaller angle of incidence and wherein said control means establishes a higher transmission frequency for the closer cell than for the remote cell.

6. Apparatus according to claim 1 wherein said antenna means illuminates a cell remote from the ground track at a large angle of incidence and illuminates at least one cell closer to the ground track at a smaller angle of incidence and wherein said receiver-transmitter means is further defined as obtaining a greater number of measurement samples from the closer cell than from the remote cell.

7. Apparatus according to claim 1 wherein said antenna means illuminates respective cells arranged transversely to the satellite ground track.

8. Apparatus according to claim 1 wherein said antenna means produces a pencil radar beam for illuminating an area comparable in shape and size to a measurement cell.

9. Apparatus according to claim 1 wherein said control means establishes a transmission frequency such that said back-scatter property is representative of a wind based parameter.