Safety level specific error response scheme for mixed criticality systems
US-9672095-B2 · Jun 6, 2017 · US
US11280916B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-11280916-B2 |
| Application number | US-201815977296-A |
| Country | US |
| Kind code | B2 |
| Filing date | May 11, 2018 |
| Priority date | Nov 12, 2015 |
| Publication date | Mar 22, 2022 |
| Grant date | Mar 22, 2022 |
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A system for receiving and processing satellite signals from satellites of global navigation systems, in particular for a vehicle, having a signal path includes a signal conditioning unit for conditioning received satellite signals, an analysis unit for analyzing the conditioned satellite signals, and a position determination unit for determining measured values utilizing the satellite signals provided by the analysis unit. The measured values include a position, a speed, and/or a satellite time. The system has two signal paths which are separate from one another and each process mutually independent satellite signals for a position.
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What is claimed is: 1. A system for determining a position of a vehicle, the system supported by the vehicle and comprising: an antenna configured to receive satellite signals from satellites of global navigation systems; a splitter for separating the satellite signals onto a first signal path and a second signal path separate and independent from the first signal path; a first signal conditioning unit for conditioning the received satellite signals along the first signal path; a second signal conditioning unit for conditioning the received satellite signals along the second signal path; a first analysis unit for analyzing the conditioned satellite signals along the first signal path; a second analysis unit for analyzing the conditioned satellite signals along the second signal path; a first position determination unit for determining measured values including at least two of a first position, a first speed, and a first satellite time utilizing the analyzed satellite signal provided by the first analysis unit, wherein the analyzed satellite signals provided by the first analysis unit are within a first frequency of a first satellite signal type; a second position determination unit for determining measured values including at least two of a second position, a second speed, and a second satellite time utilizing the analyzed satellite signals provided by the second analysis unit, wherein the analyzed satellite signals provided by the second analysis unit are within a second frequency of the first satellite signal type; and a localization unit configured to: compare the satellite signals along the first signal path with the satellite signals along the second signal path; determine an error in the satellite signals based on the comparison; determine a difference by comparing the first position and the second position; when the difference exceeds a threshold value, determine that the first signal path and/or the second signal path are subject to the error; and when the difference does not exceed the threshold value, determine the position based on the first position and the second position. 2. The system as set forth in claim 1 , wherein at least one of the analysis units is configured to separate the satellite signal on the basis of one or more signal properties and to provide the respective position determination unit with those satellite signals which are independent of the satellite signals for the other position determination unit. 3. The system as set forth in claim 1 , wherein at least one of the analysis units is configured to separate the satellite signals according to the frequencies of the satellite signals. 4. The system as set forth in claim 1 , wherein the localization unit receives the measured values determined by the position determination units and determines measured values whose plausibility has been checked. 5. The system as set forth in claim 4 , wherein the localization unit is configured to compare the determined measured values from the first position determination unit to the determined measured values from the second position determination unit to determine differences between the respective types of measured values. 6. The system as set forth in claim 4 , wherein the localization unit rejects at the first position or the second position when the difference exceeds a threshold value. 7. The system as set forth in claim 6 , wherein the threshold value is in a range of 3 m to 5 m. 8. The system as set forth in claim 4 , wherein the localization unit is configured to compare the satellite signal in the first signal path which are conditioned by the first signal conditioning unit with the satellite signal in the second signal path. 9. The system as set forth in claim 4 , wherein the localization unit is configured to compare the satellite signal in the first signal path which are conditioned by the first analysis unit with the satellite signal in the second signal path. 10. The system as set forth in claim 4 , wherein the localization unit is configured to determine a corrected position whose plausibility has been checked with the aid of alternative locating methods. 11. The system as set forth in claim 4 , wherein the localization unit is configured to create a movement trajectory on the basis of past positions whose plausibility has been checked and to identify a discontinuity between the currently determined position and the movement trajectory. 12. The system as set forth in claim 11 , wherein the localization unit is configured to extend the movement trajectory into the future utilizing odometry data. 13. A method for determining a position of a vehicle, the method comprising: receiving, at an antenna, satellite signals; distributing the satellite signals to a first signal path and a second signal path separate from the first signal path; conditioning the satellite signals along each signal path; analyzing the conditioned satellite signals along each signal path; determining a first position measured values using at least two of a first position, a first speed, and a first satellite time with a first position determination unit with the conditioned satellite signals along the first signal path, the analyzed satellite signals along the first signal path are within a first frequency of a first satellite signal type; and determining a second position measured values using at least two of a second position, a second speed, and a second satellite time with a second position determination unit with the conditioned satellite signal along the second signal path, the analyzed satellite signals along the second signal path are within a second frequency of the first satellite signal type; comparing the satellite signals along the first signal path with the satellite signals along the second signal path; determining an error in the satellite signals based on the comparison; determining a difference by comparing the first position and the second position; when the difference exceeds a threshold value, determining that the first signal path and/or the second signal path are subject to the error; and when the difference does not exceed the threshold value, determining the position based on the first position and the second position. 14. The method as set forth in claim 13 , further comprising receiving the positions determined by the position determination unit at a localization unit and determining positions whose plausibility has been checked. 15. The method as set forth in claim 13 , further comprising rejecting the determined position if the difference exceeds a threshold value.
Determining accuracy or reliability of position or pseudorange measurements · CPC title
Multimode operation in different systems which transmit time stamped messages, e.g. GPS/GLONASS · CPC title
relating to the receiver frond end · CPC title
Integrity monitoring, fault detection or fault isolation of space segment · CPC title
by combining or switching between position solutions or signals derived from different modes of operation in a single system · CPC title
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