FR3092429B1 - Piloting device intended to be integrated into a pre-existing aircraft - Google Patents
Piloting device intended to be integrated into a pre-existing aircraft Download PDFInfo
- Publication number
- FR3092429B1 FR3092429B1 FR1901190A FR1901190A FR3092429B1 FR 3092429 B1 FR3092429 B1 FR 3092429B1 FR 1901190 A FR1901190 A FR 1901190A FR 1901190 A FR1901190 A FR 1901190A FR 3092429 B1 FR3092429 B1 FR 3092429B1
- Authority
- FR
- France
- Prior art keywords
- piloting
- existing aircraft
- integrated
- instruction
- piloting device
- 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
- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 abstract 2
- 239000013589 supplement Substances 0.000 abstract 1
Classifications
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
- G05D1/0055—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots with safety arrangements
- G05D1/0061—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots with safety arrangements for transition from automatic pilot to manual pilot and vice versa
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
- B64C13/02—Initiating means
- B64C13/16—Initiating means actuated automatically, e.g. responsive to gust detectors
- B64C13/18—Initiating means actuated automatically, e.g. responsive to gust detectors using automatic pilot
Landscapes
- Engineering & Computer Science (AREA)
- Automation & Control Theory (AREA)
- Aviation & Aerospace Engineering (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Position Fixing By Use Of Radio Waves (AREA)
- Traffic Control Systems (AREA)
Abstract
Dispositif de pilotage agencé pour être intégré dans un aéronef préexistant qui comporte des systèmes d’origine comprenant un système de commandes de vol et un système de pilotage automatique, le dispositif de pilotage étant distinct et autonome par rapport aux systèmes d’origine et comprenant une unité de positionnement (27) et une unité de commande (28), l’unité de positionnement (27) étant agencée pour produire des données de positionnement de l’aéronef préexistant, l’unité de commande (28) étant agencée pour mettre en œuvre une fonction de géorepérage (70) à partir des données de positionnement produites par l’unité de positionnement (27) et pour produire une consigne de pilotage alternative (Cpa) de l’aéronef préexistant, la consigne de pilotage alternative (Cpa) étant adaptée à suppléer une consigne de pilotage manuelle produite par un pilote de l’aéronef préexistant via le système de commande de vol et une consigne de pilotage automatique produite par le système de pilotage automatique. FIGURE DE L’ABREGE : [Fig. 3]Piloting device arranged to be integrated into a pre-existing aircraft which comprises original systems comprising a flight control system and an automatic piloting system, the piloting device being separate and autonomous from the original systems and comprising a positioning unit (27) and a control unit (28), the positioning unit (27) being arranged to produce positioning data of the pre-existing aircraft, the control unit (28) being arranged to put in implements a geofencing function (70) from the positioning data produced by the positioning unit (27) and to produce an alternative piloting instruction (Cpa) of the pre-existing aircraft, the alternative piloting instruction (Cpa) being adapted to supplement a manual piloting instruction produced by a pilot of the pre-existing aircraft via the flight control system and an automatic piloting instruction produced by the autopilot system matic. ABREGE FIGURE: [Fig. 3]
Priority Applications (15)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1901190A FR3092429B1 (en) | 2019-02-06 | 2019-02-06 | Piloting device intended to be integrated into a pre-existing aircraft |
US17/416,335 US11834151B2 (en) | 2018-12-19 | 2019-12-19 | System for configuring an aircraft in a single-pilot mode or a two-pilot mode |
US17/416,346 US11945571B2 (en) | 2018-12-19 | 2019-12-19 | Piloting device designed to be integrated into a preexisting aircraft |
AU2019410275A AU2019410275A1 (en) | 2018-12-19 | 2019-12-19 | Method for piloting an aircraft |
PCT/EP2019/086279 WO2020127710A1 (en) | 2018-12-19 | 2019-12-19 | System for configuring an aircraft in a single-pilot mode or a two-pilot mode |
CN201980090873.7A CN113412217B (en) | 2018-12-19 | 2019-12-19 | A pilot device designed to be integrated into existing aircraft |
AU2019408031A AU2019408031A1 (en) | 2018-12-19 | 2019-12-19 | System for configuring an aircraft in a single-pilot mode or a two-pilot mode |
CN201980090883.0A CN113412218B (en) | 2018-12-19 | 2019-12-19 | Acquisition and analysis equipment designed to be integrated into existing aircraft |
PCT/EP2019/086269 WO2020127702A1 (en) | 2018-12-19 | 2019-12-19 | Acquisition and analysis device intended for integration into a pre-existing aircraft |
PCT/EP2019/086270 WO2020127703A1 (en) | 2018-12-19 | 2019-12-19 | Piloting device designed to be integrated into a preexisting aircraft |
US17/415,482 US12319435B2 (en) | 2018-12-19 | 2019-12-19 | Method for piloting an aircraft |
SG11202106268PA SG11202106268PA (en) | 2018-12-19 | 2019-12-19 | System for configuring an aircraft in a single-pilot mode or a two-pilot mode |
PCT/EP2019/086273 WO2020127706A1 (en) | 2018-12-19 | 2019-12-19 | Method for piloting an aircraft |
SG11202106279TA SG11202106279TA (en) | 2018-12-19 | 2019-12-19 | Method for piloting an aircraft |
US17/416,310 US12208880B2 (en) | 2018-12-19 | 2019-12-19 | Acquisition and analysis device intended for integration into a pre-existing aircraft |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1901190A FR3092429B1 (en) | 2019-02-06 | 2019-02-06 | Piloting device intended to be integrated into a pre-existing aircraft |
FR1901190 | 2019-02-06 |
Publications (2)
Publication Number | Publication Date |
---|---|
FR3092429A1 FR3092429A1 (en) | 2020-08-07 |
FR3092429B1 true FR3092429B1 (en) | 2021-01-22 |
Family
ID=67262529
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1901190A Active FR3092429B1 (en) | 2018-12-19 | 2019-02-06 | Piloting device intended to be integrated into a pre-existing aircraft |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR3092429B1 (en) |
Family Cites Families (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US10730609B2 (en) * | 2016-03-03 | 2020-08-04 | Sikorsky Aircraft Corporation | Fly-by-wire retrofit kit |
-
2019
- 2019-02-06 FR FR1901190A patent/FR3092429B1/en active Active
Also Published As
Publication number | Publication date |
---|---|
FR3092429A1 (en) | 2020-08-07 |
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Legal Events
Date | Code | Title | Description |
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PLFP | Fee payment |
Year of fee payment: 2 |
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PLSC | Publication of the preliminary search report |
Effective date: 20200807 |
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Year of fee payment: 3 |
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Year of fee payment: 4 |
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PLFP | Fee payment |
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PLFP | Fee payment |
Year of fee payment: 7 |