SATELLITE BEAM-POINTING ERROR CORRECTION IN DIGITAL BEAM-FORMING ARCHITECTURE

• US 20100231442A1
• Filed: 02/29/2008
• Published: 09/16/2010
• Est. Priority Date: 03/03/2007
• Status: Active Grant

• Current Assignee: Astrium Limited (Airbus SE)
• Original Assignee: Astrium Limited (Airbus SE)
• Inventors: Craig, Anthony Duncan, Norridge, Paul Stephen
• Granted Patent: US 8,339,307 B2
• Time in Patent Office: Days
• US Class Current: 342/354
• CPC Class Codes: H04B 7/0851 using training sequences or error signal minimizing error signal H04B7/0854
• CPC Class Codes: H04B 7/18515 Transmission equipment in satellites or space-based relays

Abstract

A digital method of determining and correcting beam-pointing for a communications spacecraft that has a digital beam-forming architecture for defining multiple spot transmit and receive beams, the antenna system of the spacecraft including a receive antenna (DRA, AFR) having antenna elements providing respective antenna element signals, and wherein at least one of the uplink signals to the spacecraft includes a beacon signal,

and wherein the method comprises digitally weighting components of said beacon signal present in antenna element signals, combining such weighted beacon signal components such as to derive beam-pointing error signals, and employing the error signals to adjust beam-forming weight values of the receive antenna, in order to adjust the pointing direction of at least one signal beam. The digital weights for the beacon signal define difference radiation patterns for x, y axes of the antenna which vary rapidly in a range corresponding to the pointing errors most commonly occurring.

Claims

1-40. -40. (canceled)

41. A method of beam-forming for an antenna of a spacecraft, the spacecraft forming part of a system that includes ground stations communicating with an antenna system of the spacecraft by means of uplink signals and downlink signals, each in a respective frequency channel, which antenna system includes a receive antenna having a plurality of antenna elements arranged in an array, each element providing a respective antenna element signal, the method comprising:

digitising each said antenna element signal, and processing each digitised antenna element signal to separate uplink signal components in respective frequency channels present in the element signal, digitally weighting, with respective beam-forming weight values, said uplink signal components in at least one frequency channel, and combining the weighted components to synthesise the uplink signal in said one frequency channel;

wherein at least one of said uplink signals includes a beacon signal, and wherein the method further comprises;

digitally weighting, with respective beam-pointing error weight values, components of said beacon signal present in at least some of the antenna element signals, and assessing such weighted beacon signal components such as to derive a beam-pointing error signal; and

employing said error signal to adjust the pointing direction of at least one communications signal beam provided by said antenna system.

43. A method according to claim 41 or 42, wherein a said antenna is a Direct Radiating Array or Imaged Phased Array, comprising an array of antenna elements providing respective element signals.

44. A method according to claim 41 or 42, wherein a said antenna is an Array Fed Reflector comprising an array of antenna elements directed at a reflector, and providing respective antenna element signals.

45. A method according to claim 41 or 42, including providing a first set of said weighted beacon signal components, and combining them to derive a first combined weighted value relating to beam-pointing error for a first axis of the receive antenna.

46. A method according to claim 45, including providing a second set of said weighted beacon signal components and combining them to derive a second combined weighted value relating to beam-pointing error for a second axis of the receive antenna, preferably orthogonal to the first axis.

47. A method according to claim 45, wherein the receive antenna is an Array Fed Reflector, and said first set and/or said second set comprises first and second weighted beacon signal components of element signals of antenna elements separated along a said axis.

48. A method according to claim 45, wherein said first set and/or second set relate to a difference radiation pattern, and the method further including providing a third set of said weighted beacon signal components, which are combined to derive a combined sum value relating to a sum radiation pattern, and normalising said first and/or second combined weighted values by division by said combined sum value, in order to derive first and/or second beam-pointing error signals.

49. A method according to claim 41 or 42, wherein the beam-pointing error weight values synthesise a difference radiation pattern along a first axis of the receive antenna, with a signal null, and with the amplitude rising on either side of the null, but with a phase difference on either side of the null.

50. A method according to claim 49 wherein the beam-pointing error weight values synthesise a difference radiation pattern along a second axis of the receive antenna, with a signal null, and with the amplitude rising on either side of the null, but with a phase difference on either side of the null.

51. A method according to claim 49, wherein the phase difference is 180°

.

52. A method according to claim 41 or 42, wherein said beam-pointing error weight values are chosen so as to synthesise a radiation pattern for the receive antenna, wherein antenna gain values change significantly for changes in beam direction, at least over a certain range of beam directions corresponding to beam-pointing errors that frequently occur.

53. A method according to claim 41 or 42, wherein said pointing direction is corrected by adjusting the attitude of the satellite in pitch and roll.

54. A method according to claim 41 or 42, wherein the pointing error is adjusted by a mechanical antenna pointing mechanism.

55. A method according to claim 41 or 42, wherein said pointing direction is corrected by adjusting said beam-forming weight values, in dependence on said error signal.

56. A method according to claim 55, wherein a said antenna is an Array Fed Reflector, and wherein said adjusting is carried out by selection of pre-computed weight sets in accordance with values of the error signal.

57. A method according to claim 41, wherein the beam that is corrected is a beam of the receive antenna.

59. A method according to claim 41 or 42, wherein an uplink communication beam from a ground station of known location also acts as a beacon for the purpose of measuring beam-pointing error.

60. A method according to claim 41 or 42, wherein a plurality of receive beams of the antenna are uncorrelated, and each uplink signal forms a respective beacon signal for the respective beam.

61. A method according to claim 41 or 42, wherein a further beacon signal is provided to provide a further error value, where the yaw angle of the space craft may create errors in addition to pitch and roll.

42. A method of beam-forming for an antenna of a spacecraft, the spacecraft forming part of a system that includes ground stations communicating with an antenna system of the spacecraft by means of uplink signals and downlink signals, each in a respective frequency channel, which antenna system includes a receive antenna and a transmit antenna, each said antenna including a plurality of antenna elements arranged in an array, each element having an associated respective antenna element signal, the method comprising:

digitising each said element signal from said receive antenna, and processing each digitised antenna element signal to separate uplink signal components in respective frequency channels present in the element signal, providing downlink signals in respective frequency channels and in digital form, which are selectively digitally weighted, with respective beam-forming weight values, to synthesise downlink antenna element signals for the antenna elements of said transmit antenna;

wherein at least one of said uplink signals includes a beacon signal, and wherein the method further comprises;

digitally weighting, with respective beam-pointing error weight values, components of said beacon signal present in at least some of the receive antenna element signals, and assessing such weighted beacon signal components such as to derive a beam-pointing error signal; and

employing said error signal to adjust the pointing direction of at least one communications signal beam provided by said transmit antenna.

58. A method according to claim 42, wherein the beam that is corrected is a beam of the transmit antenna.

62. Apparatus for forming a beam of a spacecraft antenna, comprising:

a receive antenna including a plurality of antenna elements arranged in an array, each antenna element providing a respective antenna element signal in response to received uplink signals in respective frequency channels, uplink signal synthesis means including digital processing means for digitising each said antenna element signal, and for separating uplink signal components in respective frequency channels present in each said antenna element signal, and beam-forming weighting means for digitally weighting said uplink signal components in at least one frequency channel with respective beam-forming weight values, and combining means for combining such selected components to synthesise at least one uplink signal in a respective frequency channel;

beacon direction assessment means responsive to a beacon signal comprising one of said uplink signals in a respective frequency channel, and including beam-pointing error weighting means for digitally weighting components of said beacon signal present in at least some of the antenna element signals with respective beam-pointing error weights, and for assessing the weighted beacon signal components to derive a beam-pointing error signal; and

adjustment means for employing said error signal to adjust the pointing direction of at least one communications signal beam provided by the spacecraft.

64. Apparatus according to claim 62 or 63, wherein a said antenna is a Direct Radiating Array or Imaged Phased Array, comprising an array of antenna elements providing respective element signals.

65. Apparatus according to claim 62 or 63, wherein a said antenna is an Array Fed Reflector comprising an array of antenna elements directed at a reflector, and providing respective antenna element signals.

66. Apparatus according to claim 65, wherein the receive antenna is an Array Fed Reflector, and said assessment means comprise combining means for combining first and second said weighted beacon signal components of element signals of first and second spaced apart elements to determine at least one beam-pointing error value, and normalisation means responsive to said one error value to derive said beam-pointing error signal.

67. Apparatus according to claim 62 or 63, wherein said assessment means comprise combining means for combining selected weighted beacon signal components to determine at least one beam-pointing error value, and normalisation means responsive to said one error value to derive said beam-pointing error signal.

68. Apparatus according to claim 62 or 63, wherein said beam-pointing error weighting means includes a first difference digital beam-forming network responsive to said beacon signal components, and having a first set of beam-pointing error weights for determining an x difference radiation pattern value along a first direction (x) of the antenna.

69. Apparatus according to claim 68, wherein said beam-pointing error weighting means includes a second difference digital beam-forming network responsive to said beacon signal components, and having a second set of beam-pointing error weights for determining a y difference radiation pattern value along a second direction (y) of the antenna.

70. Apparatus according to claim 68, including a further sum digital beam-forming network responsive to said beacon signal components and having a set of beam-pointing error weights for determining a sum radiation pattern value, and including normalisation means operative to divide said first and/or second difference pattern values by said sum value to provide first and/or second beam-pointing error signals.

71. Apparatus according to claim 62 or 63, wherein said beam-pointing error weight values provide a synthesized radiation pattern along one axis of the antenna array, with a signal null, and with the amplitude rising on either side of the null, but with a phase difference on either side of the null.

72. Apparatus according to claim 71, wherein the beam-pointing error weight values synthesise a radiation pattern along another axis of the antenna, with a signal null and with the amplitude rising on either side of the null, but with a phase difference on either side of the null.

73. Apparatus according to claim 62 or 63, wherein said adjusting means is operative to adjust the attitude of the satellite in pitch and roll.

74. Apparatus according to claim 62 or 63, wherein said adjusting means is operative to adjust a mechanical antenna pointing mechanism.

75. Apparatus according to claim 62 or 63, wherein said adjusting means is operative to adjust said beam-forming weight values, in dependence on said error value.

76. Apparatus according to claim 75, said adjusting means including weight control means, which acts to adjust said beam-forming weight values.

77. Apparatus according to claim 76, wherein a said antenna is an Array Fed Reflector, and wherein said adjusting means includes pre-computed weight sets, and means for selecting a weight set.

78. Apparatus according to claim 75, wherein the beam-forming weight values that are corrected relate to a beam of the receive antenna.

79. Apparatus according to claim 75, wherein the beam-forming weight values that are corrected relate to a beam of a transmit antenna.

80. Apparatus according to claim 62 or 63, including, corresponding to said beacon direction assessment means, a second beacon direction assessment means responsive to a second beacon signal for deriving a further beam-pointing error signal.

63. Apparatus for forming a beam of a spacecraft antenna, comprising:

a receive antenna and a transmit antenna, each antenna including a plurality of antenna elements arranged in an array, and each antenna element providing a respective antenna element signal in response to uplink/downlink signals in respective frequency channels, uplink signal synthesis means including digital processing means for digitising each receive antenna element signal, and for separating uplink signal components in respective frequency channels present in each said antenna element signal, downlink signal synthesis means including digital means for selectively forming downlink signals in respective frequency channels, and beam-forming weighting means for selectively digitally weighting downlink signals in respective frequency channels with respective beam-forming weight values, for providing antenna element signals to said transmit antenna;

beacon direction assessment means responsive to a beacon signal comprising one of said uplink signals in a respective frequency channel, and including beam-pointing error weighting means for digitally weighting components of said beacon signal present in at least some of the receive antenna element signals with respective beam-pointing error weights, and for assessing the weighted beacon signal components to derive a beam-pointing error signal; and

adjustment means for employing said error signal to adjust the pointing direction of at least one communications signal beam provided by the spacecraft.