Electrically scanning microwave radiometer

Claim 2

An electrically scanning microwave radiometer mounted in a flying body orbiting a planet and operative to measure a surface of the planet, said electrically scanning microwave radiometer comprising: a receiving antenna having a single radiation face a shape of which is cylindrical and is capable of scanning the surface of the planet along a conical section, the receiving antenna being constructed such that the single radiation face receives radiated energy substantially along a beam axis that extends from the radiation face to the surface of the planet; a receiver for detecting original signals received by the receiving antenna and indicating a radiation from the planet to generate detected signals; an integrator for integrating the detected signals to generate integrated signals; and measurement signal providing means for processing the integrated signals to generate measurement signals which indicate the result of measurement for the surface of the planet and will be provided to an earth station; wherein said receiving antenna comprises: a plurality of sub-arrays disposed on said single radiation face and arranged in a scan direction, each of said plurality of sub-arrays having at least one beam for receiving the radiation from the planet; a sub-array selection switch for selecting at least one of said plurality of sub-arrays as a receiving sub-array and for supplying the radiation received by the receiving sub-array to the receiver as said original signals; and switch control means for controlling said sub-array selection switch to change the receiving sub-array sequentially in the scan direction such that the surface of said planet will be scanned along said conical section.

Claim 3

An electrically scanning microwave radiometer as defined in claim 1 wherein said switch control means is operative to change the receiving sub-array sequentially in the scan direction at a speed which is determined depending on an altitude of said flying body.

Claim 4

An electrically scanning microwave radiometer as defined in claim 1 wherein the switch control means is operative to change the receiving sub-array sequentially in the scan direction at a speed lower than a speed which is determined depending on an altitude of said flying body.

Claim 5

An electrically scanning microwave radiometer as defined in claim 1 wherein said switch control means is operative to change the receiving sub-array sequentially in the scan direction at a speed higher than a speed which is determined depending on an altitude of said flying body.

Claim 6

An electrically scanning microwave radiometer as defined in claim 1 wherein each of said plurality of sub-arrays comprises: at least one radiation element for receiving the radiation from said planet, said at least one radiation element being disposed on said radiation face; at least one variable phase shifter coupled to the at least one radiation element, said at least one variable phase shifter being operative to shift the phase of the radiation received by the at least one radiation element; and phase-shift control means for controlling phase-shifts through said at least one variable phase shifter to generate a beam through said at least one radiation element and to steer said beam in the scan direction.

Claim 7

An electrically scanning microwave radiometer as defined in claim 1 wherein each of said plurality of sub-arrays comprises a plurality of radiation elements for receiving the radiation from said planet, said plurality of radiation elements being disposed on said radiation face and arranged on intersections of an imaginary lattice composed of rows parallel to the scan direction and columns perpendicular to the scan direction; a plurality of variable phase shifters each provided for the corresponding one of said columns, each of said plurality of variable phase shifters being operative to combine and shift a phase of the radiation received by radiation elements belonging to the corresponding one of said columns; and phase-shift control means for controlling phase-shifts through said plurality of variable phase shifters to generate a beam through said plurality of radiation elements and to steer said beam in the scan direction.

Claim 8

An electrically scanning microwave radiometer as defined in claim 1 wherein each of said plurality of sub-arrays comprises: a plurality of radiation elements for receiving the radiation from said planet, said plurality of radiation elements being disposed on said radiation face and arranged on intersections of an imaginary lattice composed of rows parallel to the scan direction and columns perpendicular to the scan direction; a plurality of variable phase shifters each provided for a corresponding one of said plurality of radiation elements, each of said plurality of variable phase shifters being operative to shift a phase of the radiation received by the corresponding one of said plurality of radiation elements; and phase-shift control means for controlling phase-shifts through said plurality of variable phase shifters to generate a beam through said plurality of radiation elements and to steer said beam both in the scan direction and a direction perpendicular to the scan direction.

Claim 9

An electrically scanning microwave radiometer as defined in claim 1 wherein each of said plurality of sub-arrays comprises: a plurality of radiation elements for receiving the radiation from said planet, said plurality of radiation elements being disposed on said radiation face and arranged in the scan direction; a plurality of variable phase shifters each provided for a corresponding one of said plurality of radiation elements, each of said plurality of variable phase shifters being operative to shift the phase of the radiation received by the corresponding one of said plurality of radiation elements; and phase-shift control means for controlling phase-shifts through said plurality of variable phase shifters to form an isophase plane forwardly of said plurality of sub-arrays.

Claim 10

An electrically scanning microwave radiometer as defined in claim 1 wherein each of said plurality of sub-arrays has at least two beams on a plane which is perpendicular to the scan direction and wherein one set comprising said sub-array selection switch, said receiver and said integrator are provided for each beam on the plane.

Claim 11

An electrically scanning microwave radiometer as defined in claim 1 wherein at least two radiation faces each having a cylindrical shape are provided to form a composite cylindrical face, each of said plurality of sub-arrays having a beam provided for each of said radiation faces on a plane which is perpendicular to the scan direction and wherein one set comprising said sub-array selection switch, said receiver and said integrator is provided for each beam of said plurality of sub-arrays.

Claim 12

An electrically scanning microwave radiometer as defined in claim 9 wherein at least two radiation faces each having a cylindrical shape are provided to form a composite cylindrical face, each of said plurality of sub-arrays having a beam provided for each of said radiation faces on a plane which is perpendicular to the scan direction.

Claim 13

An electrically scanning microwave radiometer as defined in claim 1 wherein said at least one beam is directed outwardly from a convex surface of said radiation face.

Claim 14

An electrically scanning microwave radiometer as defined in claim 1 wherein each of said at least one beam is directed outwardly from a concave surface of said radiation face.

Claim 15

An electrically scanning microwave radiometer as defined in claim 1, further comprising means for controlling said receiving antenna to scan the surface of said planet along a plurality of partial conical sections in parallel, the plurality of partial conical sections being provided by dividing said conical section.

Claim 16

An electrically scanning microwave radiometer as defined in claim 1 wherein said receiving antenna simultaneously receives the radiation including a plurality of polarizations, one set comprising said receiver and said integrator being provided for each of said plurality of polarizations and said electrically scanning microwave radiometer further comprising polarization separation means for separating the original signals received by said receiving antenna based on a polarization of each of the original signals and for supplying separated original signals to a corresponding one of said receivers.

Claim 17

An electrically scanning microwave radiometer as defined in claim 1 wherein said receiving antenna simultaneously receives the radiation including a plurality of frequencies, one set comprising said receiver and said integrator being provided for each of said plurality of frequencies and said electrically scanning microwave radiometer further comprising frequency separation means for separating the original signals received by said receiving antenna based on a frequency of each of the original signals and for supplying separated original signals corresponding to one of said receivers.

Claim 18

An electrically scanning microwave radiometer as defined in claim 1 wherein said receiving antenna simultaneously receives the radiation including combinations of a plurality of polarizations and a plurality of frequencies, one set comprising said receiver and said integrator being provided for each of the combinations, said electrically scanning microwave radiometer further comprising polarization and frequency separation means for separating the original signals received by said receiving antenna based on a combination of a frequency and a polarization of each of the original signals and for supplying separated original signals to a corresponding one of said receivers.

Claim 19

An electrically scanning microwave radiometer as defined in claim 1, further comprising detailed observation control means for controlling said receiving antenna such that said at least one beam slowly traces a particular area on the surface of said planet.

Claim 20

An electrically scanning microwave radiometer as defined in claim 18, further comprising means for stopping scanning by said receiving antenna as said at least one beam is tracing said particular area.

Claim 21

An electrically scanning microwave radiometer as defined in claim 1 wherein said measurement signal providing means includes means for data-compressing the integrated signals.

Claim 22

An electrically scanning microwave radiometer as defined in claim 1, wherein said flying body is an artificial satellite or planetary probe, said receiver is operative to amplify said original signals before detection and said measurement signal providing means is operative to convert the integrated signals into digital signals which are in turn formatted by said measurement signal providing means.

Claim 23

An electrically scanning microwave radiometer mounted in a flying body orbiting a planet and operative to measure a surface of the planet, said electrically scanning microwave radiometer comprising: a receiving antenna having a single radiation face a shape of which is multiplicated and is capable of scanning the surface of the planet along a conical section, the receiving antenna being constructed such that the single radiation face receives radiated energy substantially along a beam axis that extends from the radiation face to the surface of the planet; a receiver for detecting original signals received by the receiving antenna and indicating a radiation from the planet to generate detected signals; an integrator for integrating the detected signals to generate integrated signals; and measurement signal providing means for processing the integrated signals to generate measurement signals which indicate the result of measurement for the surface of the planet and will be provided to an earth station; where said receiving antenna comprises: a plurality of sub-arrays disposed on said single radiation face and arranged along a scan direction, each of said plurality of sub-arrays having at least one beam for receiving the radiation from the planet, said beam being two-dimensionally steerable both in a scan direction and a direction perpendicular to the scan direction; a sub-array selection switch for selecting at least one of said plurality of sub-arrays as a receiving sub-array, and for supplying the radiation from the planet received by the plurality of radiation elements to the receiver as the original signals; switch control means for controlling the sub-array selection switch; and beam control means for two-dimensionally steering the beam, said beam control means being co-operative with said switch control means to select one of the plurality of sub-arrays sequentially along the scan direction as the receiving sub-array such that the surface of the planet will be scanned along the conical section and also to steer the beam two-dimensionally.

Claim 24

An electrically scanning microwave radiometer mounted in a flying body orbiting a planet and operative to measure a surface of the planet, said electrically scanning microwave radiometer comprising: a receiving antenna having a single radiation face a shape of which is multiplicated and is capable of scanning the surface of the planet along a conical section, the receiving antenna being constructed such that the single radiation face receives radiated energy substantially along a beam axis that extends from the radiation face to the surface of the planet; a receiver for detecting original signals received by the receiving antenna and indicating a radiation from the planet to generate detected signals; an integrator for integrating the detected signals to generate integrated signals; and measurement signal providing means for processing the integrated signals to generate measurement signals which indicate the result of measurement for the surface of the planet and will be provided to an earth station; where said receiving antenna comprises: a plurality of sub-arrays disposed on said single radiation face and arranged along a scan direction, each of said plurality of sub-arrays having at least one beam for receiving the radiation from the planet, said beam being two-dimensionally steerable both in a scan direction and a direction perpendicular to the scan direction; a sub-array selection switch for selecting at least one of said plurality of sub-arrays as a receiving sub-array, and for supplying the radiation from the planet received by the plurality of radiation elements to the receiver as the original signals; switch control means for controlling the sub-array selection switch; and beam control means for two-dimensionally steering the beam, said beam control means being co-operative with said switch control means to select one of the plurality of sub-arrays sequentially along the scan direction as the receiving sub-array such that the surface of the planet will be scanned along the conical section and also to steer the beam two-dimensionally.

Claim 25

An electrically scanning microwave radiometer as defined in claim 22 wherein the switch control means and the beam control means select and the receiving sub-array sequentially in the scan direction and also two-dimensionally steer said beam, at a speed determined depending in an altitude of said flying body.

Claim 26

An electrically scanning microwave radiometer as defined in claim 22 wherein the switch control means and the beam control means select the receiving sub-array sequentially in the scan direction and also two-dimensionally steer said beam, at a speed lower than a speed determined depending on an altitude of said flying body.

Claim 27

An electrically scanning microwave radiometer as defined in claim 22 wherein the switch control means and the beam control means select the receiving sub-array sequentially in the scan direction and also two-dimensionally steer said beam, at a speed higher than a speed determined depending on an altitude of said flying body.

Claim 28

An electrically scanning microwave radiometer as defined in claim 22 wherein each of said plurality of sub-arrays comprises: at least one radiation element for receiving the radiation from said planet, said at least one radiation element being disposed on said radiation face; at least one variable phase shifter coupled to the at least one radiation element, the at least one variable phase shifter being operative to shift a phase of the radiation received by the at least one radiation element; and phase-shift control means for controlling phase-shifts through said at least one variable phase shifter to generate a beam through said at least one radiation element and to steer said beam in the scan direction.

Claim 29

An electrically scanning microwave radiometer as defined in claim 22 wherein each of said plurality of sub-arrays comprises: a plurality of radiation elements for receiving the radiation from said planet, said plurality of radiation elements being disposed on said radiation face and arranged on intersections of an imaginary lattice composed of rows parallel to the scan direction and columns perpendicular to the scan direction; a plurality of variable phase shifters each provided for a corresponding one of said columns, each of said plurality of variable phase shifters being operative to combine and shift a phase of the radiation received by radiation elements belonging to the corresponding one of said columns; and phase-shift control means for controlling phase-shifts through said plurality of variable phase shifters to generate a beam through said plurality of radiation elements and to steer said beam in the scan direction.

Claim 30

An electrically scanning microwave radiometer as defined in claim 22 wherein each of said sub-arrays comprises: a plurality of radiation elements for receiving the radiation from said planet, said plurality of radiation elements being disposed on said multiplicated face and arranged on intersections of an imaginary lattice compose of rows parallel to the scan direction and columns perpendicular to the scan direction; a plurality of variable phase shifters each provided for a corresponding one of said plurality of radiation elements, each of said plurality of variable phase shifters being operative to shift a phase of the radiation received by the corresponding one of said plurality of radiation elements; and phase-shift control means for controlling phase-shifts through said plurality of variable phase shifters to generate beam through said plurality of radiation elements and to steer said beam both in the scan direction and the direction perpendicular to the scan direction.

Claim 31

An electrically scanning microwave radiometer as defined in claim 22 wherein each of said plurality of sub-arrays comprises: a plurality of radiation elements for receiving the radiation from said planet, said plurality of radiation elements being disposed on said multiplicated face and arranged in a predetermined direction; a plurality of variable phase shifters each provided for corresponding one of said plurality of radiation elements, each of said plurality of variable phase shifters being operative to shift a phase of the radiation received by the corresponding one of said plurality of radiation elements; and phase-shift control means for controlling phase-shifts through said plurality of variable phase shifters to form an isophase plane forwardly of said plurality of sub-arrays.

Claim 32

An electrically scanning microwave radiometer as defined in claim 22 wherein each of said plurality of sub-arrays has at least two beams on a plane which is perpendicular to the scan direction and wherein one set comprising said sub-array selection switch, said receiver and said integrator are provided for each of said beams.

Claim 33

An electrically scanning microwave radiometer as defined in claim 30 wherein at least two radiation faces each having a multiplicated shape are provided to form a composite multiplicated face, each of said plurality of sub-arrays having a beam provided for each of said radiation faces on a plane which is perpendicular to the scan direction.

Claim 34

An electrically scanning microwave radiometer as defined in claim 22 wherein at least two radiation faces each having a multiplicated shape are provided to form a composite multiplicated face, each of said plurality of sub-arrays having a beam provided for each of said radiation faces on a plane which is perpendicular to the scan direction and wherein one set comprising said sub-array selection switch, said receiver and said integrator is provided for each beam.

Claim 35

An electrically scanning microwave radiometer as defined in claim 22 wherein said beam is directed outwardly from a convex surface of said radiation face.

Claim 36

An electrically scanning microwave radiometer as defined in claim 22 wherein said beam is directed outwardly from a concave surface of said face.

Claim 37

An electrically scanning microwave radiometer as defined in claim 1, further comprising means for controlling said receiving antenna to scan an area of the surface of said planet more than once.

Claim 38

An electrically scanning microwave radiometer as defined in claim 22, further comprising means for controlling said receiving antenna to scan an area of the surface of said planet more than once.

Claim 39

An electrically scanning microwave radiometer as defined in claim 22, further comprising means for controlling said receiving antenna to scan the surface of said planet along a plurality of partial conical sections in parallel, the plurality of partial conical sections being provided by dividing said conical section.

Claim 40

An electrically scanning microwave radiometer as defined in claim 22 wherein said receiving antenna simultaneously receives the radiation including a plurality of polarizations, one set comprising said receiver and said integrator being provided for each of said plurality of polarizations and said electrically scanning microwave radiometer further comprising polarization separation means for separating the original signals received by said receiving antenna based on a polarization of each of the original signals and for supplying separated original signals to a corresponding one of said receivers.

Claim 41

An electrically scanning microwave radiometer as defined in claim 22 wherein said receiving antenna simultaneously receives the radiation including a plurality of frequencies, one set comprising said receiver and integrator being provided for each of said plurality of frequencies and said electrically scanning microwave radiometer further comprising frequency separation means for separating the original signals received by said receiving antenna based on a frequency of each of said original signals and for supplying separated original signals corresponding to one of said receivers.

Claim 42

An electrically scanning microwave radiometer as defined in claim 22 wherein said receiving antenna simultaneously receives the radiation including combinations of a plurality of polarizations and a plurality of frequencies, one set comprising said receiver and said integrator being provided for each of the combinations, said electrically scanning microwave radiometer frequency further comprising polarization and frequency separation means for separating the original signals received by said receiving antenna based on a combination of a frequency and a polarization of each of said original signals and for supplying separated original signals to a corresponding one of said receivers.

Claim 43

An electrically scanning microwave radiometer as defined in claim 22, further comprising detailed observation control means for controlling said receiving antenna such that said at least one beam slowly traces a particular area on the surface of said planet.

Claim 44

An electrically scanning microwave radiometer as defined in claim 41, further comprising means for stopping scanning by said receiving antenna as said at least one beam is tracing said particular area.

Claim 45

An electrically scanning microwave radiometer as defined in claim 22 wherein said measurement signal providing means includes means for data-compressing the integrated signals.

Claim 46

An electrically scanning microwave radiometer defined in claim 22 wherein said flying body is an artificial satellite or planetary probe, said receiver is operative to amplify said original signals before detection and said measurement signal providing means is operative to convert the integrated signals into digital signals which are in turn formatted by said measurement signal providing means.

Claim 47

A receiving antenna for use in an electrically scanning microwave radiometer mounted in a flying body orbiting a planet and operative to measure a face of the planet, said receiving antenna comprising: a plurality of sub-arrays disposed on a cylindrical radiation face and arranged in a scan direction, each of said plurality of sub-arrays having at least one beam for receiving unreflected radiation substantially along a beam axis that extends from the radiation face to the planet; a sub-array selection switch for selecting at least one of said plurality of sub-arrays as a receiving sub-array and for supplying the radiation received by the receiving sub-array to a receiver as original signals; and switch control means for controlling the sub-array selection switch to change the receiving sub-array sequentially along the scan direction to scan the surface of the planet along a conical section.

Claim 48

A receiving antenna for use in an electrically scanning microwave radiometer mounted in a flying body orbiting a planet and operative to measure a face of the planet, said receiving antenna comprising: a plurality of sub-arrays disposed on a cylindrical radiation face and arranged in a scan direction, each of said plurality of sub-arrays having at least one beam for receiving unreflected radiation substantially along a beam axis that extends from the radiation face to the planet; a sub-array selection switch for selecting at least one of said plurality of sub-arrays as a receiving sub-array and for supplying the radiation received by the receiving sub-array to a receiver as original signals; and switch control means for controlling the sub-array selection switch to change the receiving sub-array sequentially along the scan direction to scan the surface of the planet along a conical section.

Claim 49

A receiving antenna as defined in claim 45 wherein each of said plurality of sub-arrays comprises: a plurality of radiation elements for receiving the radiation from said planet, said plurality of radiation elements being disposed on said cylindrical radiation face and arranged on intersections of an imaginary lattice composed of rows parallel to the scan direction and columns perpendicular to the scan direction; a plurality of variable phase shifters each provided for the corresponding one of said plurality of radiation elements, each of said plurality of variable phase shifters being operative to shift a phase of the radiation received by the corresponding one of said plurality of radiation elements; and phase-shift control means for controlling phase-shifts through said plurality of variable phase shifters to generate a beam through said plurality of radiation elements and to steer said beam both in the scan direction and a direction perpendicular to the scan direction.

Claim 50

A receiving antenna as defined in claim 45 wherein each of said plurality of sub-arrays has at least two beams on a plane which is perpendicular to the scan direction.

Claim 51

A receiving antenna as defined in claim 47 wherein at least two cylindrical radiation faces are provided to form a composite cylindrical face, each of said plurality of sub-arrays having a beam provided for each of said cylindrical radiation faces on a plane which is perpendicular to the scan direction.

Claim 52

A receiving antenna as defined in claim 45 wherein at least two cylindrical radiation faces are provided to form a composite cylindrical radiation face, each of said plurality of sub-arrays having a beam provided for each of said cylindrical radiation faces on a plane which is perpendicular to the scan direction.

Claim 53

A receiving antenna as defined in claim 45 wherein the beam is directed outwardly from a convex surface of said cylindrical radiation face.

Claim 54

A receiving antenna as defined in claim 45 wherein the beam is directed outwardly from a concave surface of said cylindrical radiation face.

Claim 55

A receiving antenna for use in an electrically scanning microwave radiometer mounted in a flying body orbiting a planet and operative to measure the surface of the planet, said receiving antenna comprising: a plurality of sub-arrays disposed on a multiplicated radiation face and arranged in a scan direction, each of said plurality of sub-arrays having at least one beam for receiving radiation substantially along a beam axis that extends from the radiation face to the planet, said beam being two-dimensionally steerable both in a scan direction and a direction perpendicular to the scan direction; a sub-array selection switch for selecting at least one of said plurality of sub-arrays as a receiving sub-array and for supplying the radiation received by the receiving sub-array to a receiver as original signals; switch control means for controlling the sub-array selection switch; and beam control means for two-dimensionally steering the beam, said beam control means co-operative with said switch control means to change the receiving sub-array sequentially and to steer the beam two-dimensionally such that the surface of the planet will be scanned along the conical section.

Claim 56

A receiving antenna for use in an electrically scanning microwave radiometer mounted in a flying body orbiting a planet and operative to measure the surface of the planet, said receiving antenna comprising: a plurality of sub-arrays disposed on a multiplicated radiation face and arranged in a scan direction, each of said plurality of sub-arrays having at least one beam for receiving radiation substantially along a beam axis that extends from the radiation face to the planet, said beam being two-dimensionally steerable both in a scan direction and a direction perpendicular to the scan direction; a sub-array selection switch for selecting at least one of said plurality of sub-arrays as a receiving sub-array and for supplying the radiation received by the receiving sub-array to a receiver as original signals; switch control means for controlling the sub-array selection switch; and beam control means for two-dimensionally steering the beam, said beam control means co-operative with said switch control means to change the receiving sub-array sequentially and to steer the beam two-dimensionally such that the surface of the planet will be scanned along the conical section.

Claim 57

A receiving antenna as defined in claim 52 wherein each of said plurality of sub-arrays comprises: a plurality of radiation elements for receiving the radiation from said planet, said plurality of radiation elements being disposed on said multiplicated radiation face and arranged on intersections of an imaginary lattice compose of rows parallel to the scan direction and columns perpendicular to the scan direction; a plurality of variable phase shifters each provided for the corresponding one of said plurality of radiation elements, each of said plurality of variable phase shifters being operative to shift a phase of the radiation received by the corresponding one of said plurality of elements; and phase-shift control means for controlling the phase-shifts through said plurality of variable phase shifters to generate said beams through said plurality of radiation elements and to steer said beam both in the scan direction and the direction perpendicular to the scan direction.

Claim 58

A receiving antenna as defined in claim 52 wherein each of said plurality of sub-arrays has at least two beams on a plane which is perpendicular to the scan direction.

Claim 59

A receiving antenna as defined in claim 54 wherein at least two multiplicated radiation faces are provided to form a composite multiplicated radiation face, each of said plurality of sub-arrays having a beam provided for each of said multiplicated radiation faces on a plane which is perpendicular to the scan direction.

Claim 60

A receiving antenna as defined in claim 52 wherein at least two multiplicated faces are provided to form a composite multiplicated radiation face, each of said plurality of sub-arrays having a beam provided for each of said multiplicated radiation faces on a plane which is perpendicular to the scan direction.

Claim 61

A receiving antenna as defined in claim 52 wherein said beam is directed outwardly from a convex surface of said multiplicated radiation face.

Claim 62

A receiving antenna as defined in claim 52 wherein said beam is directed outwardly from a concave surface of said multiplicated radiation face.