CA2697086C - Systeme d'atterrissage d'avion utilisant le gnss relatif - Google Patents
Systeme d'atterrissage d'avion utilisant le gnss relatif Download PDFInfo
- Publication number
- CA2697086C CA2697086C CA2697086A CA2697086A CA2697086C CA 2697086 C CA2697086 C CA 2697086C CA 2697086 A CA2697086 A CA 2697086A CA 2697086 A CA2697086 A CA 2697086A CA 2697086 C CA2697086 C CA 2697086C
- Authority
- CA
- Canada
- Prior art keywords
- base station
- mobile base
- gnss
- data
- antenna
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
- 238000000034 method Methods 0.000 claims abstract description 30
- 238000012545 processing Methods 0.000 claims abstract description 5
- 238000013459 approach Methods 0.000 claims description 70
- 238000005259 measurement Methods 0.000 claims description 36
- 230000003416 augmentation Effects 0.000 claims description 11
- 230000005540 biological transmission Effects 0.000 claims description 6
- 230000003190 augmentative effect Effects 0.000 claims description 4
- 238000012790 confirmation Methods 0.000 claims 2
- 230000002708 enhancing effect Effects 0.000 claims 1
- 238000013519 translation Methods 0.000 claims 1
- 238000010586 diagram Methods 0.000 description 11
- 238000012937 correction Methods 0.000 description 7
- 230000006870 function Effects 0.000 description 6
- 101000699762 Homo sapiens RNA 3'-terminal phosphate cyclase Proteins 0.000 description 4
- 102100029143 RNA 3'-terminal phosphate cyclase Human genes 0.000 description 4
- IWUCXVSUMQZMFG-AFCXAGJDSA-N Ribavirin Chemical compound N1=C(C(=O)N)N=CN1[C@H]1[C@H](O)[C@H](O)[C@@H](CO)O1 IWUCXVSUMQZMFG-AFCXAGJDSA-N 0.000 description 4
- 238000004422 calculation algorithm Methods 0.000 description 4
- 239000000284 extract Substances 0.000 description 3
- 238000013075 data extraction Methods 0.000 description 2
- 238000004364 calculation method Methods 0.000 description 1
- 238000004891 communication Methods 0.000 description 1
- 238000004883 computer application Methods 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 230000007613 environmental effect Effects 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 238000000691 measurement method Methods 0.000 description 1
- 238000012544 monitoring process Methods 0.000 description 1
- 230000003362 replicative effect Effects 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
Classifications
-
- G—PHYSICS
- G08—SIGNALLING
- G08G—TRAFFIC CONTROL SYSTEMS
- G08G5/00—Traffic control systems for aircraft, e.g. air-traffic control [ATC]
- G08G5/02—Automatic approach or landing aids, i.e. systems in which flight data of incoming planes are processed to provide landing data
- G08G5/025—Navigation or guidance aids
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01S—RADIO 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
- G01S19/00—Satellite radio beacon positioning systems; Determining position, velocity or attitude using signals transmitted by such systems
- G01S19/01—Satellite radio beacon positioning systems transmitting time-stamped messages, e.g. GPS [Global Positioning System], GLONASS [Global Orbiting Navigation Satellite System] or GALILEO
- G01S19/03—Cooperating elements; Interaction or communication between different cooperating elements or between cooperating elements and receivers
- G01S19/07—Cooperating elements; Interaction or communication between different cooperating elements or between cooperating elements and receivers providing data for correcting measured positioning data, e.g. DGPS [differential GPS] or ionosphere corrections
- G01S19/072—Ionosphere corrections
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01S—RADIO 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
- G01S19/00—Satellite radio beacon positioning systems; Determining position, velocity or attitude using signals transmitted by such systems
- G01S19/01—Satellite radio beacon positioning systems transmitting time-stamped messages, e.g. GPS [Global Positioning System], GLONASS [Global Orbiting Navigation Satellite System] or GALILEO
- G01S19/03—Cooperating elements; Interaction or communication between different cooperating elements or between cooperating elements and receivers
- G01S19/08—Cooperating elements; Interaction or communication between different cooperating elements or between cooperating elements and receivers providing integrity information, e.g. health of satellites or quality of ephemeris data
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot
- G05D1/04—Control of altitude or depth
- G05D1/06—Rate of change of altitude or depth
- G05D1/0607—Rate of change of altitude or depth specially adapted for aircraft
- G05D1/0653—Rate of change of altitude or depth specially adapted for aircraft during a phase of take-off or landing
- G05D1/0676—Rate of change of altitude or depth specially adapted for aircraft during a phase of take-off or landing specially adapted for landing
Abstract
Une méthode pour confirmer l'intégrité de la station de base mobile dans un système d'atterrissage d'avion utilisant le GNSS relatif, la méthode comprenant : déterminer une position relative d'une première antenne GNSS fixée à la station de base mobile par rapport à une deuxième antenne GNSS également fixée à la station de base mobile par le traitement de signaux à partir d'une constellation de satellites GNSS; calculer une distance entre la première antenne GNSS et la deuxième antenne GNSS à l'aide de la position relative mesurée; comparer une distance calculée à une distance fixe connue; et confirmer l'intégrité de la station de base mobile si la distance calculée est à un seuil prédéterminé de la distance fixe connue.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CA2697086A CA2697086C (fr) | 2010-03-17 | 2010-03-17 | Systeme d'atterrissage d'avion utilisant le gnss relatif |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CA2697086A CA2697086C (fr) | 2010-03-17 | 2010-03-17 | Systeme d'atterrissage d'avion utilisant le gnss relatif |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CA2697086A1 CA2697086A1 (fr) | 2011-09-17 |
| CA2697086C true CA2697086C (fr) | 2013-03-26 |
Family
ID=44645892
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CA2697086A Active CA2697086C (fr) | 2010-03-17 | 2010-03-17 | Systeme d'atterrissage d'avion utilisant le gnss relatif |
Country Status (1)
| Country | Link |
|---|---|
| CA (1) | CA2697086C (fr) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US11393348B1 (en) * | 2017-05-05 | 2022-07-19 | Architecture Technology Corporation | Autonomous and automatic, predictive aircraft surface state event track system and corresponding methods |
-
2010
- 2010-03-17 CA CA2697086A patent/CA2697086C/fr active Active
Also Published As
| Publication number | Publication date |
|---|---|
| CA2697086A1 (fr) | 2011-09-17 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| EEER | Examination request |