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MX2016004627A - Metodo y dispositivo para controlar un vehiculo aereo no tripulado. - Google Patents

Metodo y dispositivo para controlar un vehiculo aereo no tripulado.

Info

Publication number
MX2016004627A
MX2016004627A MX2016004627A MX2016004627A MX2016004627A MX 2016004627 A MX2016004627 A MX 2016004627A MX 2016004627 A MX2016004627 A MX 2016004627A MX 2016004627 A MX2016004627 A MX 2016004627A MX 2016004627 A MX2016004627 A MX 2016004627A
Authority
MX
Mexico
Prior art keywords
uav
unmanned aerial
distance
aerial vehicle
human
Prior art date
Application number
MX2016004627A
Other languages
English (en)
Other versions
MX368890B (es
Inventor
Xia Yongfeng
Liu Xin
Ye Hualin
Original Assignee
Xiaomi Inc
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 Xiaomi Inc filed Critical Xiaomi Inc
Publication of MX2016004627A publication Critical patent/MX2016004627A/es
Publication of MX368890B publication Critical patent/MX368890B/es

Links

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
    • G05D1/0011—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots associated with a remote control arrangement
    • 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
    • G05D1/0011—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots associated with a remote control arrangement
    • G05D1/0022—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots associated with a remote control arrangement characterised by the communication link
    • 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
    • G01S19/13—Receivers
    • G—PHYSICS
    • G08—SIGNALLING
    • G08G—TRAFFIC CONTROL SYSTEMS
    • G08G5/00—Traffic control systems for aircraft
    • G08G5/20—Arrangements for acquiring, generating, sharing or displaying traffic information
    • G08G5/26—Transmission of traffic-related information between aircraft and ground stations
    • G—PHYSICS
    • G08—SIGNALLING
    • G08G—TRAFFIC CONTROL SYSTEMS
    • G08G5/00—Traffic control systems for aircraft
    • G08G5/50—Navigation or guidance aids
    • G08G5/55—Navigation or guidance aids for a single aircraft
    • G—PHYSICS
    • G08—SIGNALLING
    • G08G—TRAFFIC CONTROL SYSTEMS
    • G08G5/00—Traffic control systems for aircraft
    • G08G5/50—Navigation or guidance aids
    • G08G5/57—Navigation or guidance aids for unmanned aircraft
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U2101/00—UAVs specially adapted for particular uses or applications
    • B64U2101/20—UAVs specially adapted for particular uses or applications for use as communications relays, e.g. high-altitude platforms
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U2101/00—UAVs specially adapted for particular uses or applications
    • B64U2101/30—UAVs specially adapted for particular uses or applications for imaging, photography or videography
    • 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
    • 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
    • G05D1/02—Control of position or course in two dimensions
    • G05D1/021—Control of position or course in two dimensions specially adapted to land vehicles
    • G05D1/0212—Control of position or course in two dimensions specially adapted to land vehicles with means for defining a desired trajectory
    • G05D1/0214—Control of position or course in two dimensions specially adapted to land vehicles with means for defining a desired trajectory in accordance with safety or protection criteria, e.g. avoiding hazardous areas
    • 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
    • G05D1/02—Control of position or course in two dimensions
    • G05D1/021—Control of position or course in two dimensions specially adapted to land vehicles
    • G05D1/0231—Control of position or course in two dimensions specially adapted to land vehicles using optical position detecting means
    • 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
    • G05D1/10—Simultaneous control of position or course in three dimensions

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Automation & Control Theory (AREA)
  • Computer Networks & Wireless Communication (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Traffic Control Systems (AREA)
  • Selective Calling Equipment (AREA)

Abstract

La presente invención se refiere a un método para controlar un Vehículo Aéreo No Tripulado y un dispositivo del mismo, los cuales pertenecen a Vehículos Aéreos No Tripulados (UAV) del campo de la seguridad. El método incluye: determinar si una distancia entre un Vehículo Aéreo No Tripulado (UAV) y su controlador va más allá de la distancia de visión del humano; detectar si un enlace de retorno de datos de un sistema externo del UAV es normal; y cuando la distancia entre el UAV y el controlador va más allá de la distancia de visión del humano y el enlace de retorno de datos del sistema externo es anormal, controlar el UAV para entrar en un modo de protección de retorno. El dispositivo incluye un módulo de determinación, un módulo de detección y un módulo de control. Cuando la distancia entre el UAV y el controlador va más allá de la distancia de visión del humano y los datos de enlace de retorno del sistema externo son anormales, es difícil para los usuarios determinar el entorno de vuelo el UAV. En tal caso, controlar el UAV para entra en un modo de protección de retorno puede proteger el UAV, lo que lleva a la reducción de la posibilidad de que el UAV choque con los objetos que lo rodean y mejora la seguridad del UAV.
MX2016004627A 2015-10-30 2015-12-25 Metodo y dispositivo para controlar un vehiculo aereo no tripulado. MX368890B (es)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
CN201510727596.XA CN105278544B (zh) 2015-10-30 2015-10-30 无人飞行器的控制方法及装置
PCT/CN2015/098844 WO2017071044A1 (zh) 2015-10-30 2015-12-25 无人飞行器的控制方法及装置

Publications (2)

Publication Number Publication Date
MX2016004627A true MX2016004627A (es) 2017-08-09
MX368890B MX368890B (es) 2019-10-21

Family

ID=55147722

Family Applications (1)

Application Number Title Priority Date Filing Date
MX2016004627A MX368890B (es) 2015-10-30 2015-12-25 Metodo y dispositivo para controlar un vehiculo aereo no tripulado.

Country Status (8)

Country Link
US (1) US20170123413A1 (es)
EP (1) EP3163394B1 (es)
JP (1) JP6400225B2 (es)
KR (1) KR20170061624A (es)
CN (1) CN105278544B (es)
MX (1) MX368890B (es)
RU (1) RU2637838C2 (es)
WO (1) WO2017071044A1 (es)

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Also Published As

Publication number Publication date
RU2016114286A (ru) 2017-10-16
CN105278544B (zh) 2018-05-08
JP6400225B2 (ja) 2018-10-03
EP3163394A1 (en) 2017-05-03
US20170123413A1 (en) 2017-05-04
MX368890B (es) 2019-10-21
JP2017539040A (ja) 2017-12-28
CN105278544A (zh) 2016-01-27
WO2017071044A1 (zh) 2017-05-04
EP3163394B1 (en) 2020-02-12
KR20170061624A (ko) 2017-06-05
RU2637838C2 (ru) 2017-12-07

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