METHOD FOR MONITORING AND CONSOLIDATING A SATELLITE NAVIGATION SOLUTION
A consolidation method implementing: a first sensor able to determine a computed position {circumflex over (x)}(1) of the aircraft, a characterization of the positioning error and a horizontal protection level HPL(1), a second sensor, with a different design and with a design level equivalent to the...
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Main Authors | , , |
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Format | Patent |
Language | English French German |
Published |
25.10.2023
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Subjects | |
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Abstract | A consolidation method implementing: a first sensor able to determine a computed position {circumflex over (x)}(1) of the aircraft, a characterization of the positioning error and a horizontal protection level HPL(1), a second sensor, with a different design and with a design level equivalent to the first sensor, able to determine a second position {circumflex over (x)}(2) of the aircraft and a characterization of the positioning error of the second position {circumflex over (x)}(2), and comprising the steps: a. estimating a horizontal deviation between the computed position {circumflex over (x)}(1) and the second position {circumflex over (x)}(2), b. comparing the horizontal deviation with a detection threshold, c. if the horizontal deviation is below the detection threshold, computing an additional horizontal protection level HPL(MON) of the computed position {circumflex over (x)}(1), d. estimating a consolidated horizontal protection level HPL(CON), e. comparing the consolidated horizontal protection level HPL(CON) and a horizontal alert limit HAL, f. if the consolidated horizontal protection level HPL(CON) is less than the horizontal alert limit HAL, horizontally confirming the computed position {circumflex over (x)}(1). |
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AbstractList | A consolidation method implementing: a first sensor able to determine a computed position {circumflex over (x)}(1) of the aircraft, a characterization of the positioning error and a horizontal protection level HPL(1), a second sensor, with a different design and with a design level equivalent to the first sensor, able to determine a second position {circumflex over (x)}(2) of the aircraft and a characterization of the positioning error of the second position {circumflex over (x)}(2), and comprising the steps: a. estimating a horizontal deviation between the computed position {circumflex over (x)}(1) and the second position {circumflex over (x)}(2), b. comparing the horizontal deviation with a detection threshold, c. if the horizontal deviation is below the detection threshold, computing an additional horizontal protection level HPL(MON) of the computed position {circumflex over (x)}(1), d. estimating a consolidated horizontal protection level HPL(CON), e. comparing the consolidated horizontal protection level HPL(CON) and a horizontal alert limit HAL, f. if the consolidated horizontal protection level HPL(CON) is less than the horizontal alert limit HAL, horizontally confirming the computed position {circumflex over (x)}(1). |
Author | BOUVET, Denis MEHLEN, Christian BONEL, Roland |
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DocumentTitleAlternate | VERFAHREN ZUR ÜBERWACHUNG UND KONSOLIDIERUNG EINER SATELLITENNAVIGATIONSLÖSUNG PROCEDE DE SURVEILLANCE ET DE CONSOLIDATION D'UNE SOLUTION DE NAVIGATION SATELLITAIRE |
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Snippet | A consolidation method implementing: a first sensor able to determine a computed position {circumflex over (x)}(1) of the aircraft, a characterization of the... |
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SubjectTerms | ANALOGOUS ARRANGEMENTS USING OTHER WAVES DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES GYROSCOPIC INSTRUMENTS LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION ORRERADIATION OF RADIO WAVES MEASURING MEASURING DISTANCES, LEVELS OR BEARINGS NAVIGATION PHOTOGRAMMETRY OR VIDEOGRAMMETRY PHYSICS RADIO DIRECTION-FINDING RADIO NAVIGATION SURVEYING TESTING |
Title | METHOD FOR MONITORING AND CONSOLIDATING A SATELLITE NAVIGATION SOLUTION |
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