FIELD: location indication error and integrity assessment.
SUBSTANCE: invention relates to location indication error and integrity assessment. The technical result is achieved by recording the position values (P-N, P-2, P-1) and calculating the receiver clock error by means of the satellite navigation system (SNS) discrete time measurement transit time, recording the first pseudodistance before the later moment of time by means of time discrete transit time measurement using SNS, extrapolating the receiver position values (P'0) at a later moment of time based on a trajectory that replicates the receiver's previous path, extrapolating the receiver clock error at a later moment of time based on a number of clock errors calculated before the later moment of time, determining the distance (r'0) between the extrapolated value (P'0) of the receiver position and the SNS satellite position (S0) at a later moment of time, at the same time, the satellite positioning capability quality level is achieved by forming a second pseudodistance based on the sum of the determined distance (r'0) and the extrapolated clock error at a later moment of time and comparing the second pseudodistance with the first pseudodistance.
EFFECT: invention improves the location indication error and integrity assessment quality.
12 cl, 1 dwg
Title | Year | Author | Number |
---|---|---|---|
GEAR DETERMINING RELATIVE POSITION OF MOVING OBJECT BY SIGNALS OF SATELLITE RADIO NAVIGATION SYSTEMS WITH HIGH ACCURACY | 1998 |
|
RU2143123C1 |
METHOD OF IDENTIFYING PARAMETERS OF NAVIGATION SATELLITES | 2015 |
|
RU2584541C1 |
METHOD OF DETERMINING INTEGRITY OF HIGH-PRECISION NAVIGATION DETERMINATIONS OF CONSUMER AND SYSTEM THEREFOR | 2014 |
|
RU2577846C1 |
METHOD OF LOCATING USER TERMINALS MOVING IN COVERAGE AREA OF LOCAL NAVIGATION SYSTEM | 2023 |
|
RU2825248C1 |
METHOD OF HIGH-PRECISION NAVIGATIONAL SIGHTINGS INTEGRITY DEFINITION IN REAL TIME | 2017 |
|
RU2644450C1 |
METHOD OF DETERMINING LOCATION OF OBJECT WITH USE OF GLOBAL NAVIGATION SATELLITE SYSTEMS AND SYSTEM FOR ITS IMPLEMENTATION | 2012 |
|
RU2492499C1 |
METHOD AND SYSTEM FOR VERIFICATION OF MEASUREMENT DATA | 2015 |
|
RU2692093C2 |
METHOD OF IDENTIFYING PARAMETERS OF NAVIGATION SATELLITES | 2015 |
|
RU2587666C1 |
COARSE DETERMINATION FOR THE HYBRID NAVIGATION SOLUTION BASED ON MAGNETIC-CALIBRATED MEASUREMENTS | 2015 |
|
RU2673504C2 |
METHOD OF DETERMINING MAXIMUM USABLE FREQUENCY FOR IONOSPHERIC RADIO COMMUNICATION | 2012 |
|
RU2516239C2 |
Authors
Dates
2023-02-07—Published
2020-06-17—Filed