FR3128298B1 - Système d'aide à l'atterrissage sur une zone d'atterrissage pour un aéronef à voilure tournante - Google Patents
Système d'aide à l'atterrissage sur une zone d'atterrissage pour un aéronef à voilure tournante Download PDFInfo
- Publication number
- FR3128298B1 FR3128298B1 FR2111147A FR2111147A FR3128298B1 FR 3128298 B1 FR3128298 B1 FR 3128298B1 FR 2111147 A FR2111147 A FR 2111147A FR 2111147 A FR2111147 A FR 2111147A FR 3128298 B1 FR3128298 B1 FR 3128298B1
- Authority
- FR
- France
- Prior art keywords
- landing
- landing zone
- rotary wing
- wing aircraft
- assistance system
- 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
- 230000003287 optical effect Effects 0.000 abstract 3
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D45/00—Aircraft indicators or protectors not otherwise provided for
- B64D45/04—Landing aids; Safety measures to prevent collision with earth's surface
- B64D45/08—Landing aids; Safety measures to prevent collision with earth's surface optical
-
- 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
- G05D1/04—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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/02—Aircraft not otherwise provided for characterised by special use
- B64C39/024—Aircraft not otherwise provided for characterised by special use of the remote controlled vehicle type, i.e. RPV
-
- 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
- G01S13/00—Systems using the reflection or reradiation of radio waves, e.g. radar systems; Analogous systems using reflection or reradiation of waves whose nature or wavelength is irrelevant or unspecified
- G01S13/86—Combinations of radar systems with non-radar systems, e.g. sonar, direction finder
- G01S13/867—Combination of radar systems with cameras
-
- 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
- G01S13/00—Systems using the reflection or reradiation of radio waves, e.g. radar systems; Analogous systems using reflection or reradiation of waves whose nature or wavelength is irrelevant or unspecified
- G01S13/88—Radar or analogous systems specially adapted for specific applications
- G01S13/91—Radar or analogous systems specially adapted for specific applications for traffic control
- G01S13/913—Radar or analogous systems specially adapted for specific applications for traffic control for landing purposes
-
- 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
- G01S13/00—Systems using the reflection or reradiation of radio waves, e.g. radar systems; Analogous systems using reflection or reradiation of waves whose nature or wavelength is irrelevant or unspecified
- G01S13/88—Radar or analogous systems specially adapted for specific applications
- G01S13/93—Radar or analogous systems specially adapted for specific applications for anti-collision purposes
- G01S13/933—Radar or analogous systems specially adapted for specific applications for anti-collision purposes of aircraft or spacecraft
-
- G—PHYSICS
- G06—COMPUTING; CALCULATING OR COUNTING
- G06T—IMAGE DATA PROCESSING OR GENERATION, IN GENERAL
- G06T7/00—Image analysis
- G06T7/70—Determining position or orientation of objects or cameras
- G06T7/73—Determining position or orientation of objects or cameras using feature-based methods
- G06T7/74—Determining position or orientation of objects or cameras using feature-based methods involving reference images or patches
-
- G—PHYSICS
- G08—SIGNALLING
- G08G—TRAFFIC CONTROL SYSTEMS
- G08G5/00—Traffic control systems for aircraft, e.g. air-traffic control [ATC]
- G08G5/0017—Arrangements for implementing traffic-related aircraft activities, e.g. arrangements for generating, displaying, acquiring or managing traffic information
- G08G5/0021—Arrangements for implementing traffic-related aircraft activities, e.g. arrangements for generating, displaying, acquiring or managing traffic information located in the aircraft
-
- G—PHYSICS
- G08—SIGNALLING
- G08G—TRAFFIC CONTROL SYSTEMS
- G08G5/00—Traffic control systems for aircraft, e.g. air-traffic control [ATC]
- G08G5/0073—Surveillance aids
- G08G5/0086—Surveillance aids for monitoring terrain
-
- 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
- G06—COMPUTING; CALCULATING OR COUNTING
- G06T—IMAGE DATA PROCESSING OR GENERATION, IN GENERAL
- G06T2207/00—Indexing scheme for image analysis or image enhancement
- G06T2207/10—Image acquisition modality
- G06T2207/10032—Satellite or aerial image; Remote sensing
-
- G—PHYSICS
- G06—COMPUTING; CALCULATING OR COUNTING
- G06T—IMAGE DATA PROCESSING OR GENERATION, IN GENERAL
- G06T2207/00—Indexing scheme for image analysis or image enhancement
- G06T2207/30—Subject of image; Context of image processing
- G06T2207/30181—Earth observation
- G06T2207/30184—Infrastructure
Landscapes
- Engineering & Computer Science (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Physics & Mathematics (AREA)
- Aviation & Aerospace Engineering (AREA)
- General Physics & Mathematics (AREA)
- Computer Networks & Wireless Communication (AREA)
- Electromagnetism (AREA)
- Computer Vision & Pattern Recognition (AREA)
- Theoretical Computer Science (AREA)
- Mechanical Engineering (AREA)
- Automation & Control Theory (AREA)
- Position Fixing By Use Of Radio Waves (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
- Traffic Control Systems (AREA)
- Radar Systems Or Details Thereof (AREA)
- Navigation (AREA)
Abstract
L’invention concerne un Système d'aide à l'atterrissage sur une zone d'atterrissage pour un aéronef à voilure tournante, le système comprenant un calculateur (1), une IHM (2) pour interagir avec le pilote de l’aéronef, un ensemble optique (3) muni d'au moins un capteur optique, un ensemble radar(4) muni d'au moins un détecteur radar, et une centrale inertielle (5), dans lequel le calculateur est configuré pour mettre en œuvre les étapes suivantes : - une première étape (Etape1) consistant à déterminer une image optique de la zone d'atterrissage possible; - une deuxième étape (Etape2) consistant à déterminer la position relative de la zone d'atterrissage par rapport audit système dans le référentiel terrestre; - une troisième étape (Etape3) consistant à déterminer un chemin d’approche de la zone d’atterrissage; et - une quatrième étape (Etape4) consistant à fournir à l’IHM (2) un écart entre la position du système et le chemin d’approche. Figure pour l’abrégé : Fig. 3
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR2111147A FR3128298B1 (fr) | 2021-10-20 | 2021-10-20 | Système d'aide à l'atterrissage sur une zone d'atterrissage pour un aéronef à voilure tournante |
US17/968,696 US20230117700A1 (en) | 2021-10-20 | 2022-10-18 | Landing zone landing assistance system for a rotary wing aircraft |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR2111147 | 2021-10-20 | ||
FR2111147A FR3128298B1 (fr) | 2021-10-20 | 2021-10-20 | Système d'aide à l'atterrissage sur une zone d'atterrissage pour un aéronef à voilure tournante |
Publications (2)
Publication Number | Publication Date |
---|---|
FR3128298A1 FR3128298A1 (fr) | 2023-04-21 |
FR3128298B1 true FR3128298B1 (fr) | 2024-05-03 |
Family
ID=80787346
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR2111147A Active FR3128298B1 (fr) | 2021-10-20 | 2021-10-20 | Système d'aide à l'atterrissage sur une zone d'atterrissage pour un aéronef à voilure tournante |
Country Status (2)
Country | Link |
---|---|
US (1) | US20230117700A1 (fr) |
FR (1) | FR3128298B1 (fr) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2018027338A1 (fr) * | 2016-08-06 | 2018-02-15 | SZ DJI Technology Co., Ltd. | Évaluation automatique du terrain de surfaces d'atterrissage, et systèmes et procédés associés |
Family Cites Families (17)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR1103890A (fr) | 1954-07-08 | 1955-11-08 | Rasoir de sûreté à lame réglable | |
FR2852686B1 (fr) | 2003-03-19 | 2005-08-05 | Airbus France | Systeme de pilotage d'un aeronef, au moins pour piloter l'aeronef lors d'une approche de non precision en vue d'un atterrissage. |
US9568919B2 (en) * | 2012-10-24 | 2017-02-14 | Aurora Flight Sciences Corporation | System and methods for automatically landing aircraft |
FR3046224B1 (fr) * | 2015-12-23 | 2018-06-08 | Thales | Procede de representation graphique tridimensionnelle d'un axe de piste d'atterrissage |
US9745078B2 (en) * | 2016-02-01 | 2017-08-29 | Honeywell International Inc. | Systems and methods of precision landing for offshore helicopter operations using spatial analysis |
US20190291863A1 (en) * | 2016-05-18 | 2019-09-26 | A^3 By Airbus Llc | Vertical takeoff and landing aircraft with tilted-wing configurations |
US20190003840A1 (en) * | 2016-08-30 | 2019-01-03 | Faraday&Future Inc. | Map registration point collection with mobile drone |
FR3058555B1 (fr) * | 2016-11-10 | 2021-02-12 | Thales Sa | Uniformisation des approches plateforme pour aeronef |
FR3062720B1 (fr) * | 2017-02-08 | 2019-03-15 | Airbus Helicopters | Systeme et procede d'aide a l'atterrissage d'un aeronef, et aeronef correspondant |
US10599138B2 (en) * | 2017-09-08 | 2020-03-24 | Aurora Flight Sciences Corporation | Autonomous package delivery system |
US11866198B2 (en) * | 2018-10-29 | 2024-01-09 | California Institute Of Technology | Long-duration, fully autonomous operation of rotorcraft unmanned aerial systems including energy replenishment |
FR3107388B1 (fr) * | 2020-02-14 | 2022-03-04 | Airbus Helicopters | Procédé et système d’aide à la navigation pour un aéronef par détection d’objets maritimes en vue d’un vol d’approche, d’une mise en vol stationnaire ou d’un atterrissage |
US11535394B2 (en) * | 2020-08-10 | 2022-12-27 | The Boeing Company | Aircraft landing assistance method and memory storage device including instructions for performing an aircraft landing assistance method |
US11667390B2 (en) * | 2020-10-23 | 2023-06-06 | Ami Industries, Inc. | Systems for aircraft landing after ejection |
US11987382B2 (en) * | 2021-02-17 | 2024-05-21 | Merlin Labs, Inc. | Method for aircraft localization and control |
CN113359782B (zh) * | 2021-05-28 | 2022-07-29 | 福建工程学院 | 一种融合lidar点云与图像数据的无人机自主选址降落方法 |
US12007790B2 (en) * | 2021-06-09 | 2024-06-11 | Ford Global Technologies, Llc | Systems and methods for service drone landing zone operations |
-
2021
- 2021-10-20 FR FR2111147A patent/FR3128298B1/fr active Active
-
2022
- 2022-10-18 US US17/968,696 patent/US20230117700A1/en active Pending
Also Published As
Publication number | Publication date |
---|---|
FR3128298A1 (fr) | 2023-04-21 |
US20230117700A1 (en) | 2023-04-20 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US10473783B2 (en) | Laser processing device and laser processing system | |
FR3128298B1 (fr) | Système d'aide à l'atterrissage sur une zone d'atterrissage pour un aéronef à voilure tournante | |
JP4446195B2 (ja) | レーザ光出力部、レーザ光入力部およびレーザ式ガス分析計 | |
FR3062720B1 (fr) | Systeme et procede d'aide a l'atterrissage d'un aeronef, et aeronef correspondant | |
EP3415862B1 (fr) | Tête de palpage pour machine de mesure de coordonnées utilisant un matériau photoluminescent pour mesurer le déplacement du palpeur | |
SE458395B (sv) | Anordning foer att bestaemma riktningen av en siktlinje | |
JP2012525578A (ja) | 光学的車両レーザ検出システム | |
CN110398749B (zh) | 一种双斜射非对称车载激光测速装置 | |
FR3063712A1 (fr) | Dispositif de pilotage automatique d'un aeronef a voilure tournante et aeronef a voilure tournante comprenant un tel dispositif | |
US10267650B2 (en) | Demodulation phase calibration | |
EP2103898B1 (fr) | Procédé d'évaluation de la distance entre l'interféromètre laser de type suivi et la cible, et interféromètre laser de type suivi | |
FR3079299B1 (fr) | Dispositif de mesure des caracteristiques d'un flux d'air | |
EP1605229B1 (fr) | Instrument d'arpentage | |
EP2775722A2 (fr) | Dispositif de projection laser | |
EP1936326A1 (fr) | Système d'équilibrage spectral et procédé pour réduire le bruit dans des gyroscopes à fibres optiques | |
US11378510B2 (en) | Fine particle measuring device and fine particle measuring method | |
FR3089286B1 (fr) | Procédé et système pour mesurer une surface d’un objet comprenant des structures différentes par interférométrie à faible cohérence | |
JPWO2015132880A1 (ja) | 測定装置及び測定方法 | |
US20020113964A1 (en) | Particle size distribution measuring apparatus | |
FR3060116A1 (fr) | Systeme et procede d'affichage d'un aeronef | |
FR3049072A1 (fr) | Systeme d'affichage tete haute d'un aeronef | |
FR3102755B1 (fr) | Procédé d’aide au pilotage d’un aéronef | |
FR3103897B1 (fr) | Dispositif et procédé de mesure des angles d’orientation d’un système d’imagerie x | |
US9753049B1 (en) | Collinear system to determine its own displacement from its own motion | |
FR3110142B1 (fr) | Dispositif électronique, et procédé, de guidage du pilote dans le pilotage d'un aéronef lors de l'atterrissage en présence de vent de travers |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PLFP | Fee payment |
Year of fee payment: 2 |
|
PLSC | Publication of the preliminary search report |
Effective date: 20230421 |
|
PLFP | Fee payment |
Year of fee payment: 3 |