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1. DE102020119803 - Präzisionsanflug- und Landesystem für Luftfahrzeuge

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Office
Germany
Application Number 102020119803
Application Date 28.07.2020
Publication Number 102020119803
Publication Date 03.02.2022
Publication Kind A1
IPC
G01S 19/15
GPHYSICS
01MEASURING; TESTING
SRADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
19Satellite radio beacon positioning systems; Determining position, velocity or attitude using signals transmitted by such systems
01Satellite radio beacon positioning systems transmitting time-stamped messages, e.g. GPS , GLONASS or GALILEO
13Receivers
14specially adapted for specific applications
15Aircraft landing systems
G01S 19/07
GPHYSICS
01MEASURING; TESTING
SRADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
19Satellite radio beacon positioning systems; Determining position, velocity or attitude using signals transmitted by such systems
01Satellite radio beacon positioning systems transmitting time-stamped messages, e.g. GPS , GLONASS or GALILEO
03Cooperating elements; Interaction or communication between different cooperating elements or between cooperating elements and receivers
07providing data for correcting measured positioning data, e.g. DGPS or ionosphere corrections
CPC
G01S 19/071
GPHYSICS
01MEASURING; TESTING
SRADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
19Satellite radio beacon positioning systems; Determining position, velocity or attitude using signals transmitted by such systems
01Satellite radio beacon positioning systems transmitting time-stamped messages, e.g. GPS [Global Positioning System], GLONASS [Global Orbiting Navigation Satellite System] or GALILEO
03Cooperating elements; Interaction or communication between different cooperating elements or between cooperating elements and receivers
07providing data for correcting measured positioning data, e.g. DGPS [differential GPS] or ionosphere corrections
071DGPS corrections
G01S 19/15
GPHYSICS
01MEASURING; TESTING
SRADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
19Satellite radio beacon positioning systems; Determining position, velocity or attitude using signals transmitted by such systems
01Satellite radio beacon positioning systems transmitting time-stamped messages, e.g. GPS [Global Positioning System], GLONASS [Global Orbiting Navigation Satellite System] or GALILEO
13Receivers
14specially adapted for specific applications
15Aircraft landing systems
G01S 19/41
GPHYSICS
01MEASURING; TESTING
SRADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
19Satellite radio beacon positioning systems; Determining position, velocity or attitude using signals transmitted by such systems
38Determining a navigation solution using signals transmitted by a satellite radio beacon positioning system
39the satellite radio beacon positioning system transmitting time-stamped messages, e.g. GPS [Global Positioning System], GLONASS [Global Orbiting Navigation Satellite System] or GALILEO
40Correcting position, velocity or attitude
41Differential correction, e.g. DGPS [differential GPS]
Applicants Airbus Defence and Space GmbH
Inventors Erfinder wird später genannt werden
Agents LKGLOBAL | Lorenz & Kopf PartG mbB Patentanwälte
Title
(DE) Präzisionsanflug- und Landesystem für Luftfahrzeuge
front page image
Abstract
(DE)

Es ist ein Luftfahrzeug (100) mit einem Missionscomputer (110), einem GNSS-Empfänger (120) und einer Kommunikationsschnittstelle (130), welche ausgestaltet ist, Daten über einen verschlüsselten, bidirektionalen Kommunikationspfad zu empfangen, beschrieben. Der Missionscomputer bestimmt einen Positionswert für das Luftfahrzeug basierend auf von dem GNSS-Empfänger empfangenen Satellitensignalen, auf welche ein Korrekturterm angewandt wurde, welcher dem Luftfahrzeug über die Kommunikationsschnittstelle übermittelt wird, um korrigierte Satellitensignale zu ermitteln. Die korrigierten Satellitensignale dienen als Basis für das Ermitteln eines korrigierten Positionswertes Der Missionscomputer greift auf einen GNSS-Empfänger und eine Kommunikationsschnittstelle zurück, welche Bestandteil des Luftfahrzeugs sind, so dass zum Ermitteln der korrigierten Satellitensignale keine gesonderte Hardware-Baugruppe erforderlich ist. Daneben ist eine Bodenanordnung mit einer zugehörigen Bodenstation und optional mit einer Prüfeinheit zum Überprüfen der korrekten Bestimmung des korrigierten Positionswertes beschrieben.


Related patent documents
WO/2022/023310
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