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A system and method for determining the roll rate and roll angle of a spinning platform in a jamming environment, by suppressing the interference signals from the received GPS signals and using the measured phase and amplitude differences between the GPS satellite signals received on two or more ant

A system and method for determining the roll rate and roll angle of a spinning platform in a jamming environment, by suppressing the interference signals from the received GPS signals and using the measured phase and amplitude differences between the GPS satellite signals received on two or more antennas. The measured signal differences and the navigation solution from a GPS receiver are processed in a roll filter to obtain the desired information. Data from non-GPS measurement sources is optionally provided to update the navigation solution. Although of wide applicability, the invention is uniquely suited to the measurement of roll rates and roll angles of fast spinning platforms with small baselines in the presence of jamming, and where the antennas are separated from each other by distances that are a fraction of the GPS signal wavelength.

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1. A system for determining the roll rate and roll angle of a spinning platform comprising: at least two antennas for receiving GPS signals from at least one satellite, each antenna having an antenna channel;an antijam filter for suppressing interference signals received with the GPS signals in the

1. A system for determining the roll rate and roll angle of a spinning platform comprising: at least two antennas for receiving GPS signals from at least one satellite, each antenna having an antenna channel;an antijam filter for suppressing interference signals received with the GPS signals in the antenna channels;a GPS receiver for forming the navigation solution; anda roll processor for processing the navigation solution and the filtered GPS signals. 2. The system of claim 1, wherein the antennas are pointed in different directions. 3. The system of claim 2, wherein the antennas are circumferentially disposed on the platform about its spin axis. 4. The system of claim 1, wherein the spacing between the antennas is a fraction of the GPS signal wavelength. 5. The system of claim 1, wherein the roll processor is driven by the GPS receiver. 6. The system of claim 5, wherein processing includes correlating the filtered GPS signals. 7. The system of claim 6, wherein processing further includes measuring the differences between the correlated GPS signals. 8. The system of claim 7, wherein the roll processor includes a roll filter. 9. The system of claim 8, wherein the roll filter is a Kalman filter. 10. The system of claim 9, wherein the Kalman filter includes an Extended Kalman Filter. 11. The system of claim 8, wherein the differences between the correlated GPS signals include phase differences and amplitude differences. 12. The system of claim 8, wherein the differences between the correlated GPS signals include phase differences. 13. The system of claim 8, wherein the differences between the correlated GPS signals include amplitude differences. 14. The system of claim 8, wherein the roll filter employs a probabilistic data association (PDA) algorithm. 15. The system of claim 8, wherein the antijam filter computes the covariance matrix and its inverse using data sampled on the multiple antenna channels. 16. The system of claim 15, wherein the inverse matrix is multiplied by a steering vector to compute antijam weights. 17. The system of claim 16, wherein suppressing the interference signals includes applying the antijam weights to the data from which the inverse covariance matrix was calculated. 18. The system of claim 17, wherein processing the navigation solution and the filtered GPS signals includes inputting the inverse matrix into the roll filter. 19. A system for determining the roll rate and roll angle of a spinning platform comprising: at least two antennas for receiving GPS signals from at least one satellite, each antenna having an antenna channel;an antijam filter for suppressing interference signals received with the GPS signals in the antenna channels;a GPS receiver for forming the navigation solution; andmeans for processing the navigation solution and filtered GPS signals. 20. The system of claim 19, wherein the antennas are pointed in different directions. 21. The system of claim 20, wherein the antennas are circumferentially disposed on the platform about its spin axis. 22. The system of claim 19, wherein the spacing between the antennas is a fraction of the GPS signal wavelength. 23. The system of claim 19, wherein means for processing the navigation solution and filtered GPS signals includes a roll processor driven by the GPS receiver. 24. The system of claim 23, wherein means for processing further includes means for correlating the filtered GPS signals. 25. The system of claim 24, wherein means for processing further includes means for measuring the differences between the correlated GPS signals. 26. The system of claim 25, wherein the roll processor includes a roll filter. 27. The system of claim 26, wherein the roll filter is a Kalman filter. 28. The system of claim 27, wherein the Kalman filter includes an Extended Kalman Filter. 29. The system of claim 26, wherein the differences between the correlated GPS signals include phase differences and amplitude differences. 30. The system of claim 26, wherein the differences between the correlated GPS signals include phase differences. 31. The system of claim 26, wherein the differences between the correlated GPS signals include amplitude differences. 32. The system of claim 26, wherein the roll filter employs a probabilistic data association (PDA) algorithm. 33. The system of claim 26, wherein the antijam filter computes the covariance matrix and its inverse using data sampled on the multiple antenna channels. 34. The system of claim 33, wherein the inverse matrix is multiplied by a steering vector to compute antijam weights. 35. The system of claim 34, wherein suppressing the interference signals includes applying the antijam weights to the data from which the inverse covariance matrix was calculated. 36. The system of claim 35, wherein means for processing the navigation solution and the filtered GPS signals further includes inputting the inverse matrix into the roll filter. 37. A system for determining the roll rate and roll angle of a spinning platform comprising: at least two antennas for receiving GPS signals from at least one satellite, each antenna having an antenna channel;an antijam filter for suppressing interference signals received with the GPS signals in the antenna channels;a GPS receiver for forming the navigation solution;at least one non-GPS measurement source for updating the navigation solution; anda roll processor for processing the updated navigation solution and the filtered GPS signals. 38. The system of claim 37, wherein the antennas are pointed in different directions. 39. The system of claim 38, wherein the antennas are circumferentially disposed on the platform about its spin axis. 40. The system of claim 37, wherein the spacing between the antennas is a fraction of the GPS signal wavelength. 41. The system of claim 37, wherein the roll processor is driven by the GPS receiver. 42. The system of claim 41, wherein processing the updated navigation solution and the filtered GPS signals includes correlating the filtered GPS signals. 43. The system of claim 42, wherein processing further includes measuring the differences between the correlated GPS signals. 44. The system of claim 43, wherein the roll processor includes a roll filter. 45. The system of claim 44, wherein the roll filter is a Kalman filter. 46. The system of claim 45, wherein the Kalman filter includes an Extended Kalman Filter. 47. The system of claim 44, wherein the differences between the correlated GPS signals include phase differences and amplitude differences. 48. The system of claim 44, wherein the differences between the correlated GPS signals include phase differences. 49. The system of claim 44, wherein the differences between the correlated GPS signals include amplitude differences. 50. The system of claim 44, wherein the roll filter employs a probabilistic data association (PDA) algorithm. 51. The system of claim 44, wherein the antijam filter computes the covariance matrix and its inverse using data sampled on the multiple antenna channels. 52. The system of claim 51, wherein the inverse matrix is multiplied by a steering vector to compute antijam weights. 53. The system of claim 52, wherein suppressing the interference signals includes applying the antijam weights to the data from which the inverse covariance matrix was calculated. 54. The system of claim 53, wherein processing the updated navigation solution and the filtered GPS signals includes inputting the inverse matrix into the roll filter. 55. The system of claim 44, wherein the non-GPS measurement source is an inertial measurement unit. 56. The system of claim 44, wherein the non-GPS measurement source is a magnetometer. 57. A method for determining the roll rate and roll angle of a spinning platform comprising the steps of: receiving GPS signals from at least one satellite on at least two antennas, each antenna having an antenna channel;suppressing the interference signals received with the GPS signals in the antenna channels using an antijam filter;forming the navigation solution using a GPS receiver; andprocessing the navigation solution and filtered GPS signals. 58. The method of claim 57, wherein the antennas are pointed in different directions. 59. The method of claim 58, wherein the antennas are circumferentially disposed on the platform about its spin axis. 60. The method of claim 57, wherein the spacing between the antennas is a fraction of the GPS signal wavelength. 61. The method of claim 57, wherein processing the navigation solution and filtered GPS signals includes using a roll processor driven by the GPS receiver. 62. The method of claim 61, wherein processing further includes correlating the filtered GPS signals. 63. The method of claim 62, wherein processing further includes measuring the differences between the correlated GPS signals. 64. The method of claim 63, wherein the roll processor includes a roll filter. 65. The method of claim 64, wherein the roll filter is a Kalman filter. 66. The method of claim 65, wherein the Kalman filter includes an Extended Kalman Filter. 67. The method of claim 64, wherein the differences between the correlated GPS signals include phase differences and amplitude differences. 68. The method of claim 64, wherein the differences between the correlated GPS signals include phase differences. 69. The method of claim 64, wherein the differences between the correlated GPS signals include amplitude differences. 70. The method of claim 64, wherein the roll filter employs a probabilistic data association (PDA) algorithm. 71. The method of claim 64, wherein the antijam filter computes the covariance matrix and its inverse using data sampled on the multiple antenna channels. 72. The method of claim 71, wherein the inverse matrix is multiplied by a steering vector to compute antijam weights. 73. The method of claim 72, wherein suppressing the interference signals further includes applying the antijam weights to the data from which the inverse covariance matrix was calculated. 74. The method of claim 73, wherein processing the navigation solution and the filtered GPS signals includes inputting the inverse matrix into the roll filter. 75. A method for determining the roll rate and roll angle of a spinning platform comprising the steps of receiving GPS signals from at least one satellite on at least two antennas, each antenna having an antenna channel;suppressing the interference signals received with the GPS signals in the antenna channels using an antijam filter;forming the navigation solution using a GPS receiver;updating the navigation solution using at least one non-GPS measurement source; andprocessing the updated navigation solution and filtered GPS signals. 76. The method of claim 75, wherein the antennas are pointed in different directions. 77. The method of claim 76, wherein the antennas are circumferentially disposed on the platform about its spin axis. 78. The method of claim 75, wherein the spacing between the antennas is a fraction of the GPS signal wavelength. 79. The method of claim 75, wherein processing the updated navigation solution and filtered GPS signals includes using a roll processor driven by the GPS receiver. 80. The method of claim 79, wherein processing further includes correlating the filtered GPS signals. 81. The method of claim 80, wherein processing further includes measuring the differences between the correlated GPS signals. 82. The method of claim 81, wherein the roll processor includes a roll filter. 83. The method of claim 82, wherein the roll filter is a Kalman filter. 84. The method of claim 83, wherein the Kalman filter includes an Extended Kalman Filter. 85. The method of claim 82, wherein the differences between the correlated GPS signals include phase differences and amplitude differences. 86. The method of claim 82, wherein the differences between the correlated GPS signals include phase differences. 87. The method of claim 82, wherein the differences between the correlated GPS signals include amplitude differences. 88. The method of claim 82, wherein the roll filter employs a probabilistic data association (PDA) algorithm. 89. The method of claim 82, wherein the antijam filter computes the covariance matrix and its inverse using data sampled on the multiple antenna channels. 90. The method of claim 89, wherein the inverse matrix is multiplied by a steering vector to compute antijam weights. 91. The method of claim 90, wherein suppressing the interference signals further includes applying the antijam weights to the data from which the inverse covariance matrix was calculated. 92. The method of claim 91, wherein processing the updated navigation solution and the filtered GPS signals includes inputting the inverse matrix into the roll filter. 93. The method of claim 82, wherein the non-GPS measurement source is an inertial measurement unit. 94. The method of claim 82, wherein the non-GPS measurement source is a magnetometer.