ES2722325T3 - Sistema y método de terminación de vuelo para vehículos aéreos - Google Patents

Sistema y método de terminación de vuelo para vehículos aéreos Download PDF

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Publication number
ES2722325T3
ES2722325T3 ES15382256T ES15382256T ES2722325T3 ES 2722325 T3 ES2722325 T3 ES 2722325T3 ES 15382256 T ES15382256 T ES 15382256T ES 15382256 T ES15382256 T ES 15382256T ES 2722325 T3 ES2722325 T3 ES 2722325T3
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ES
Spain
Prior art keywords
unmanned aerial
microcontroller unit
aerial vehicle
flight
parachute
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
Application number
ES15382256T
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English (en)
Inventor
Eduardo Gabriel Ferreyra
Enrique Emilio Serrot
José Luis Lemus
José Antonio Blanco
Nieves Lapena
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Boeing Co
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Boeing Co
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Filing date
Publication date
Application filed by Boeing Co filed Critical Boeing Co
Application granted granted Critical
Publication of ES2722325T3 publication Critical patent/ES2722325T3/es
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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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
    • B64D25/00—Emergency apparatus or devices, not otherwise provided for
    • 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
    • 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
    • B64D17/00—Parachutes
    • B64D17/80—Parachutes in association with aircraft, e.g. for braking thereof
    • H—ELECTRICITY
    • H04—ELECTRIC COMMUNICATION TECHNIQUE
    • H04L—TRANSMISSION OF DIGITAL INFORMATION, e.g. TELEGRAPHIC COMMUNICATION
    • H04L67/00—Network arrangements or protocols for supporting network services or applications
    • H04L67/01—Protocols
    • H04L67/12—Protocols specially adapted for proprietary or special-purpose networking environments, e.g. medical networks, sensor networks, networks in vehicles or remote metering networks
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U2201/00—UAVs characterised by their flight controls
    • B64U2201/10—UAVs characterised by their flight controls autonomous, i.e. by navigating independently from ground or air stations, e.g. by using inertial navigation systems [INS]
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U2201/00—UAVs characterised by their flight controls
    • B64U2201/20—Remote controls
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U70/00—Launching, take-off or landing arrangements
    • B64U70/80—Vertical take-off or landing, e.g. using rockets
    • B64U70/83—Vertical take-off or landing, e.g. using rockets using parachutes, balloons or the like

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Business, Economics & Management (AREA)
  • Emergency Management (AREA)
  • Health & Medical Sciences (AREA)
  • Computing Systems (AREA)
  • General Health & Medical Sciences (AREA)
  • Medical Informatics (AREA)
  • Computer Networks & Wireless Communication (AREA)
  • Signal Processing (AREA)
  • Traffic Control Systems (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)

Abstract

Un sistema a bordo de terminación de vuelo para vehículos aéreos no tripulados que comprende un paracaídas en donde el sistema comprende al menos una unidad de microcontrolador conectada a un sistema de despliegue del paracaídas, en donde el sistema comprende sensores internos conectados a la al menos una unidad de microcontrolador, en donde los sensores internos están configurados para medir el vuelo y las variables relacionadas con vehículos aéreos no tripulados, en donde la unidad de microcontrolador está configurada para activar el sistema de despliegue del paracaídas y desplegar (8) el paracaídas del vehículo aéreo no tripulado cuando esta determina una emergencia importante durante el vuelo del vehículo aéreo no tripulado, y en donde la unidad de microcontrolador está configurada para determinar una emergencia importante con base en la comparación, con valores predeterminados, de datos comprendidos dentro de señales detectadas que comprenden mediciones tomadas por cualquier combinación de sensores internos y sensores externos; en donde los sensores externos comprenden cualquier combinación de uno o más de al menos: - sensores que no forman parte del sistema de terminación de vuelo a bordo y con los cuales un vehículo aéreo está equipado convencionalmente, ubicados a bordo del vehículo aéreo; - sensores ubicados fuera del vehículo aéreo no tripulado, conectados a la al menos una unidad de microcontrolador a través de radio; en donde la al menos una unidad de microcontrolador está configurada para: - enviar una alerta (14) a un piloto manual, a un piloto automático o a una estación de control que supervisa el vuelo, si la unidad de microcontrolador detecta que una medición tomada por cualquier combinación de los sensores internos y externos está fuera de los límites de primer rango predeterminados y dentro de límites de rango crítico predeterminados, y verificar la detección (7) de instrucciones con el fin de desplegar el paracaídas del vehículo aéreo no tripulado, en donde la unidad de microcontrolador está configurada para, si se reciben instrucciones con el fin de desplegar el paracaídas del vehículo aéreo no tripulado, activar el sistema de despliegue del paracaídas y desplegar (8) el paracaídas del vehículo aéreo no tripulado, terminando así el vuelo (9), y; - activar el sistema de despliegue del paracaídas y desplegar (8) el paracaídas del vehículo aéreo no tripulado si detecta que la medición realizada por cualquier combinación de sensores internos y externos está fuera de los límites de rango crítico predeterminados; caracterizado porque el sistema comprende un transmisor de radio configurado para conectar, a través de radio, la al menos una unidad de microcontrolador con el piloto manual ubicado fuera del vehículo aéreo no tripulado o la estación de control ubicada fuera del vehículo aéreo no tripulado; en donde el sistema está configurado para: evaluar si la transmisión de radio entre la al menos una unidad de microcontrolador y el piloto manual o la estación de control está habilitada; y si la transmisión de radio entre la al menos una unidad de microcontrolador y el piloto manual o la estación de control se desactiva, continuando el vuelo de manera autónoma hasta que se recupere dicha transmisión de radio.
ES15382256T 2015-05-18 2015-05-18 Sistema y método de terminación de vuelo para vehículos aéreos Active ES2722325T3 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
EP15382256.4A EP3095705B1 (en) 2015-05-18 2015-05-18 System and method of flight termination for air vehicles

Publications (1)

Publication Number Publication Date
ES2722325T3 true ES2722325T3 (es) 2019-08-09

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Family Applications (1)

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ES15382256T Active ES2722325T3 (es) 2015-05-18 2015-05-18 Sistema y método de terminación de vuelo para vehículos aéreos

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US (1) US10450077B2 (es)
EP (1) EP3095705B1 (es)
ES (1) ES2722325T3 (es)

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Publication number Publication date
EP3095705B1 (en) 2019-01-02
US10450077B2 (en) 2019-10-22
US20160340049A1 (en) 2016-11-24
EP3095705A1 (en) 2016-11-23

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