SELECTED ASPECTS OF ADVANCED RECEIVER AUTONOMOUS INTEGRITY MONITORING APPLICATION TO KALMAN FILTER BASED NAVIGATION FILTER
First Claim
1. A method of integrity monitoring for errors in a navigation system, the method comprising:
- receiving a plurality of signals transmitted from a plurality of spaced-based satellites;
determining a full position solution for the navigation system based on the plurality of signals;
determining one or more position sub-solutions for the navigation system based on the plurality of signals;
setting a value for a pseudorange bias;
computing a transformation matrix for the full solution and all sub-solutions using a Kalman filter;
computing a bias effect on an error of a filtered state vector component for all sub-solutions; and
adding the bias effect on the error of the filtered state vector component to computed protection levels for both vertical and horizontal dimensions.
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Abstract
A method of advanced receiver autonomous integrity monitoring of a navigation system is discussed and two modifications facilitating its implementation in a hybrid navigation system are disclosed. In the first approach, relations describing the effect of unmodeled biases in pseudo-measurement on the Kalman filter state estimate are analytically derived and their incorporation into the integrity monitoring algorithm is described. The method comprises receiving a plurality of signals transmitted from spaced-based satellites, determining a position full-solution and sub-solutions, specifying a pseudorange bias, computing a transformation matrix for the full-solution and all sub-solutions using a Kalman filter, computing a bias effect on an error of filtered state vectors of all sub-solutions, and adding the effect to computed vertical and horizontal protection levels. In the second approach, a modification for computationally effective calculation of the protection levels of hybrid navigation systems based on both integrity and non-integrity assured pseudorange error descriptions is disclosed.
21 Citations
20 Claims
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1. A method of integrity monitoring for errors in a navigation system, the method comprising:
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receiving a plurality of signals transmitted from a plurality of spaced-based satellites; determining a full position solution for the navigation system based on the plurality of signals; determining one or more position sub-solutions for the navigation system based on the plurality of signals; setting a value for a pseudorange bias; computing a transformation matrix for the full solution and all sub-solutions using a Kalman filter; computing a bias effect on an error of a filtered state vector component for all sub-solutions; and adding the bias effect on the error of the filtered state vector component to computed protection levels for both vertical and horizontal dimensions. - View Dependent Claims (2, 3, 4, 5)
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6. A method of integrity monitoring for errors in a navigation system, the method comprising:
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receiving a plurality of signals transmitted from a plurality of spaced-based satellites; determining a full position solution for the navigation system based on the plurality of signals; determining one or more position sub-solutions for the navigation system based on the plurality of signals; computing a variance of a vertical position for the full position solution with a state estimation filter based on an integrity assured error definition; computing a variance of a vertical position for the full position solution with the state estimation filter based on a non-integrity assured error definition; computing a variance of the vertical position for all position sub-solutions with one or more additional state estimation filters based on the integrity assured error definition; computing a multiplying coefficient; and computing an approximate variance of the vertical position for all position sub-solutions based on the non-integrity assured error definition and the multiplying coefficient. - View Dependent Claims (7, 8, 9, 10, 11)
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12. A navigation system, comprising:
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one or more inertial sensors that generate inertial measurements; a receiver configured to receive a plurality of signals transmitted from a plurality of spaced-based satellites; and a processor operatively coupled to the receiver and the inertial sensors, the processor configured to perform a method of integrity monitoring implemented as part of an advanced receiver autonomous integrity monitoring algorithm. - View Dependent Claims (13, 14, 15, 16, 17, 18, 19, 20)
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Specification