ES2482265B1 - Sistema de control de aeronaves no tripuladas de ala rotatoria para aterrizaje vertical en superficies móviles mediante pre-alimentacion de fuerzas en el sistema de control - Google Patents

Sistema de control de aeronaves no tripuladas de ala rotatoria para aterrizaje vertical en superficies móviles mediante pre-alimentacion de fuerzas en el sistema de control Download PDF

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Publication number
ES2482265B1
ES2482265B1 ES201232073A ES201232073A ES2482265B1 ES 2482265 B1 ES2482265 B1 ES 2482265B1 ES 201232073 A ES201232073 A ES 201232073A ES 201232073 A ES201232073 A ES 201232073A ES 2482265 B1 ES2482265 B1 ES 2482265B1
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ES
Spain
Prior art keywords
control system
aircraft
cable
untripulated
forces
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
ES201232073A
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English (en)
Other versions
ES2482265A1 (es
Inventor
Konstantin KONDAK
Manuel BÉJAR DOMÍNGUEZ
Anibal Ollero Baturone
Luis Alberto SANDINO VELÁSQUEZ
Daniel SANTAMARÍA RUBIO
Antonio JIMÉNEZ BELLIDO
Francisco ALARCÓN ROMERO
Luis Antidio VIGURIA JIMÉNEZ
Carlos ALBO SÁNCHEZ-BEDOYA
Allan ANDERSON BELL SEILER
Pablo GIL MONTAÑO
Silvia DE LOS SANTOS TRIGO
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Universidad de Sevilla
Universidad Pablo de Olavide
Fundacion Andaluza para el Desarrollo Aeroespacial
Original Assignee
Universidad de Sevilla
Universidad Pablo de Olavide
Fundacion Andaluza para el Desarrollo Aeroespacial
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Universidad de Sevilla, Universidad Pablo de Olavide, Fundacion Andaluza para el Desarrollo Aeroespacial filed Critical Universidad de Sevilla
Priority to ES201232073A priority Critical patent/ES2482265B1/es
Priority to PCT/ES2013/070935 priority patent/WO2014102437A1/es
Publication of ES2482265A1 publication Critical patent/ES2482265A1/es
Application granted granted Critical
Publication of ES2482265B1 publication Critical patent/ES2482265B1/es
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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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
    • G05D1/04—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
    • G05D1/0684—Rate of change of altitude or depth specially adapted for aircraft during a phase of take-off or landing specially adapted for landing on a moving platform, e.g. aircraft carrier
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U10/00—Type of UAV
    • B64U10/10—Rotorcrafts
    • B64U10/17—Helicopters
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U10/00—Type of UAV
    • B64U10/60—Tethered aircraft
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U70/00—Launching, take-off or landing arrangements
    • B64U70/90—Launching from or landing on platforms
    • B64U70/92—Portable platforms
    • 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
    • G05D1/08—Control of attitude, i.e. control of roll, pitch, or yaw
    • G05D1/0808—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft
    • G05D1/0866—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft specially adapted to captive aircraft
    • 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
    • B64U2201/202—Remote controls using tethers for connecting to ground station

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Remote Sensing (AREA)
  • Mechanical Engineering (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Automation & Control Theory (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Lift-Guide Devices, And Elevator Ropes And Cables (AREA)

Abstract

Mejora del sistema de control para el aterrizaje de una aeronave VTOL no tripulada sobre una plataforma móvil, consistente en la adición de un sistema de control basado en unos sensores, que miden la tensión del cable que une la aeronave con la plataforma de aterrizaje y los ángulos de orientación de dicho cable con respecto a un sistema asociado a la aeronave, y un módulo de control que toma como entradas la tensión —tanto en magnitud como en dirección-, obtenida de los citados sensores, además de las consignas de control generadas por el controlador de la aeronave. El módulo de control objeto de la invención calcula, a partir de la tensión en el cable, correcciones a introducir en las consignas de control, que se adelantan a las perturbaciones que se producirán en la posición de la aeronave como consecuencia de los cambios en la tensión del cable.

Description

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Claims (1)

  1. imagen1
    imagen2
ES201232073A 2012-12-31 2012-12-31 Sistema de control de aeronaves no tripuladas de ala rotatoria para aterrizaje vertical en superficies móviles mediante pre-alimentacion de fuerzas en el sistema de control Active ES2482265B1 (es)

Priority Applications (2)

Application Number Priority Date Filing Date Title
ES201232073A ES2482265B1 (es) 2012-12-31 2012-12-31 Sistema de control de aeronaves no tripuladas de ala rotatoria para aterrizaje vertical en superficies móviles mediante pre-alimentacion de fuerzas en el sistema de control
PCT/ES2013/070935 WO2014102437A1 (es) 2012-12-31 2013-12-30 Sistema de control de aeronaves no tripuladas de ala rotatoria para aterrizaje vertical en superficies móviles mediante pre-alimentacion de fuerzas en el sistema de control

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
ES201232073A ES2482265B1 (es) 2012-12-31 2012-12-31 Sistema de control de aeronaves no tripuladas de ala rotatoria para aterrizaje vertical en superficies móviles mediante pre-alimentacion de fuerzas en el sistema de control

Publications (2)

Publication Number Publication Date
ES2482265A1 ES2482265A1 (es) 2014-08-01
ES2482265B1 true ES2482265B1 (es) 2015-05-20

Family

ID=51019937

Family Applications (1)

Application Number Title Priority Date Filing Date
ES201232073A Active ES2482265B1 (es) 2012-12-31 2012-12-31 Sistema de control de aeronaves no tripuladas de ala rotatoria para aterrizaje vertical en superficies móviles mediante pre-alimentacion de fuerzas en el sistema de control

Country Status (2)

Country Link
ES (1) ES2482265B1 (es)
WO (1) WO2014102437A1 (es)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105138012A (zh) * 2015-09-09 2015-12-09 南京航空航天大学 一种gps引导的无人机自动着舰自适应控制系统及方法
US9841757B2 (en) 2015-12-03 2017-12-12 At&T Intellectual Property I, L.P. Drone piggybacking on vehicles
DE102018106463B4 (de) * 2018-03-20 2020-09-24 Deutsches Zentrum für Luft- und Raumfahrt e.V. Verfahren zur automatischen Unterstützung des Landens eines Luftfahrzeuges, Computerprogramm und System dafür
DE102018106462B4 (de) * 2018-03-20 2020-09-24 Deutsches Zentrum für Luft- und Raumfahrt e.V. Verfahren zur automatischen Unterstützung des Landens eines Luftfahrzeuges, Computerprogramm und System dafür
RU2725640C1 (ru) * 2019-09-09 2020-07-03 Закрытое акционерное общество "АйТи Десижн" Способ захода на посадку беспилотного летательного аппарата в аварийных условиях
WO2021170667A1 (en) * 2020-02-24 2021-09-02 Arrowtec Gmbh Tethered unmanned aerial vehicle system

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1063652A (en) * 1964-10-23 1967-03-30 Mini Of Aviat London Ground handling equipment for vertical take off and landing aircraft
FR2502772A1 (fr) * 1981-03-24 1982-10-01 Durand Bernard Procede et dispositif de mesure des trois coordonnees d'un aeronef en point fixe par rapport a un point au sol
FR2937010B1 (fr) * 2008-10-13 2010-12-10 Dcns Procede et systeme de controle de l'appontage/decollage automatique d'un drone sur ou d'une grille circulaire d'appontage d'une plate-forme notamment navale
US9387940B2 (en) * 2010-11-09 2016-07-12 Colorado Seminary Which Owns And Operates The University Of Denver Intelligent self-leveling docking system

Also Published As

Publication number Publication date
WO2014102437A1 (es) 2014-07-03
ES2482265A1 (es) 2014-08-01

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