BRPI0418602A - sistema de controle para veìculos - Google Patents

sistema de controle para veìculos

Info

Publication number
BRPI0418602A
BRPI0418602A BRPI0418602-8A BRPI0418602A BRPI0418602A BR PI0418602 A BRPI0418602 A BR PI0418602A BR PI0418602 A BRPI0418602 A BR PI0418602A BR PI0418602 A BRPI0418602 A BR PI0418602A
Authority
BR
Brazil
Prior art keywords
aircraft
control system
sensors
receiver
reference vehicle
Prior art date
Application number
BRPI0418602-8A
Other languages
English (en)
Inventor
Kenneth E Builta
James E Harris
Jeffrey W Epp
Bryan P Honza
Kynn J Schulte
Original Assignee
Bell Helicopter Textron 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
Family has litigation
First worldwide family litigation filed litigation Critical https://patents.darts-ip.com/?family=35197176&utm_source=google_patent&utm_medium=platform_link&utm_campaign=public_patent_search&patent=BRPI0418602(A) "Global patent litigation dataset” by Darts-ip is licensed under a Creative Commons Attribution 4.0 International License.
Application filed by Bell Helicopter Textron Inc filed Critical Bell Helicopter Textron Inc
Publication of BRPI0418602A publication Critical patent/BRPI0418602A/pt

Links

Classifications

    • 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
    • B64C13/20—Initiating means actuated automatically, e.g. responsive to gust detectors using radiated signals
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U70/00—Launching, take-off or landing arrangements
    • B64U70/60—Take-off or landing of UAVs from a runway using their own power
    • 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
    • G05D1/0027—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 involving a plurality of vehicles, e.g. fleet or convoy travelling
    • 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
    • B64U2201/00—UAVs characterised by their flight controls
    • 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
    • B64U80/00—Transport or storage specially adapted for UAVs
    • B64U80/80—Transport or storage specially adapted for UAVs by vehicles
    • B64U80/84—Waterborne vehicles

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Remote Sensing (AREA)
  • Automation & Control Theory (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Transportation (AREA)
  • Mechanical Engineering (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Navigation (AREA)
  • Traffic Control Systems (AREA)
  • Toys (AREA)

Abstract

SISTEMA DE CONTROLE PARA VEìCULOS. Um sistema para controle de vóo de uma aeronave apresenta sensores (37, 43), um receptor (45), e um sistema de controle digital (57), todos dos quais sendo conduzidos a bordo da aeronave. Os sensores (37, 43) determinan a posição da aeronave em relação à terra e o movimento inercial da aeronave. O receptor (45) recebe dados transmitidos (51, 55)que comunicam a posição e movimento de um veículo de referência em relação à terra. O sistema de controle (57) calcula a posição e velocidade calculada da aeronave em relação do veículo de referência usando os dados a partir dos sensores (37, 43) e receptor (45) e, em seguida, comanda dos dispositivos de controle de vóo (33) na aeronave para manobra da aeronave em uma maneira que mantém uma posição selecionada e/ou velocidade em relação ao veículo de referência. O sistema permite o uso de interfaces de usuário gráfica ou tátil.
BRPI0418602-8A 2004-03-25 2004-03-25 sistema de controle para veìculos BRPI0418602A (pt)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PCT/US2004/009080 WO2005103939A1 (en) 2004-03-25 2004-03-25 Control system for vehicles

Publications (1)

Publication Number Publication Date
BRPI0418602A true BRPI0418602A (pt) 2007-05-02

Family

ID=35197176

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0418602-8A BRPI0418602A (pt) 2004-03-25 2004-03-25 sistema de controle para veìculos

Country Status (7)

Country Link
US (2) US8014909B2 (pt)
EP (1) EP1728176B1 (pt)
CN (1) CN1934562B (pt)
BR (1) BRPI0418602A (pt)
CA (1) CA2555836C (pt)
DE (1) DE04821913T1 (pt)
WO (1) WO2005103939A1 (pt)

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US8949011B2 (en) * 2005-09-14 2015-02-03 Novatel Inc. Helicopter ship board landing system
FR2913666A1 (fr) * 2006-10-03 2008-09-19 Daniel Lafitte Aide au guidage d'un aeronef sans pilote de type minidrome par retour d'informations stipulant sa position
US7818100B2 (en) * 2007-04-03 2010-10-19 The Boeing Company System and method for optimized runway exiting
US8234021B2 (en) * 2007-06-20 2012-07-31 Honeywell International Inc. Synthetic instrument landing system
US8200375B2 (en) 2008-02-12 2012-06-12 Stuckman Katherine C Radio controlled aircraft, remote controller and methods for use therewith
US20110035150A1 (en) * 2009-08-07 2011-02-10 Gm Global Technology Operations, Inc. Simple technique for dynamic path planning and collision avoidance
FR2952033B1 (fr) * 2009-11-03 2011-12-02 Thales Sa Jauge de vitesse relative destinee au controle d'un avion sans pilote
FR2952734A1 (fr) * 2009-11-13 2011-05-20 Thales Sa Dispositif d'aide a la decision d'appontage d'un aeronef sur un navire
FR2952616B1 (fr) * 2009-11-13 2011-12-02 Thales Sa Dispositif de securisation d'une sequence de vol d'un aeronef sans pilote
US8712607B2 (en) * 2009-12-07 2014-04-29 Sikorsky Aircraft Corporation Systems and methods for velocity profile based approach to point control
EP2363343A1 (en) * 2010-02-24 2011-09-07 Eurocopter Deutschland GmbH System for control of unmanned aerial vehicles
IL204509A (en) * 2010-03-15 2015-01-29 Israel Aerospace Ind Ltd Vtol aircraft landing system
TWI459234B (zh) * 2010-07-14 2014-11-01 Hon Hai Prec Ind Co Ltd 手持裝置及利用其控制無人飛行載具的方法
DE102010055905A1 (de) 2010-09-30 2012-04-05 Liebherr-Aerospace Lindenberg Gmbh Hochauftriebssystem eines Luftfahrzeuges
CN102650888B (zh) * 2011-02-25 2016-02-10 鸿富锦精密工业（深圳）有限公司 无人飞行载具及其控制方法
US8376268B1 (en) 2012-04-09 2013-02-19 Paul Robert Otto Flight control system using thrust devices
FR2990528B1 (fr) * 2012-05-11 2015-12-25 Airbus Operations Sas Procede de commande de pilotage d'un aeronef
US8976043B2 (en) * 2012-08-20 2015-03-10 Textron Innovations, Inc. Illuminated sidestick controller, such as an illuminated sidestick controller for use in aircraft
US9568919B2 (en) * 2012-10-24 2017-02-14 Aurora Flight Sciences Corporation System and methods for automatically landing aircraft
IL225152A0 (en) * 2013-03-11 2013-06-27 Igor Teller Launching a drone from a moving platform
US9223314B2 (en) * 2013-03-14 2015-12-29 Aglunction, LLC Hovering control for helicopters using a GNSS vector
US9547991B2 (en) 2013-05-23 2017-01-17 Honeywell International Inc. Aircraft precision approach and shipboard landing control system and method
CN105938369B (zh) 2013-06-25 2018-11-02 深圳市大疆创新科技有限公司 飞行器的控制系统及控制方法
US9643722B1 (en) 2014-02-28 2017-05-09 Lucas J. Myslinski Drone device security system
US12271955B2 (en) 2014-02-28 2025-04-08 Lucas J. Myslinski Drone device
CN107409051B (zh) 2015-03-31 2021-02-26 深圳市大疆创新科技有限公司 用于生成飞行管制的认证系统和方法
JP6459014B2 (ja) 2015-03-31 2019-01-30 エスゼット ディージェイアイ テクノロジー カンパニー リミテッドＳｚ Ｄｊｉ Ｔｅｃｈｎｏｌｏｇｙ Ｃｏ．，Ｌｔｄ ジオフェンシング装置
CN107533331B (zh) * 2015-03-31 2022-07-12 深圳市大疆创新科技有限公司 具有动态特性的地理围栏设备
CN104898699B (zh) * 2015-05-28 2020-03-17 小米科技有限责任公司 飞行控制方法及装置、电子设备
EP3291042A1 (en) * 2016-09-01 2018-03-07 Sikorsky Aircraft Corporation Autonomous helicopter posture regulation to moving reference frames
WO2019084506A1 (en) * 2017-10-27 2019-05-02 Fluidity Technologies, Inc. CONTROL DEVICE EQUIPPED WITH A DISPLAY DEVICE FOR KNOWING THE SITUATION
US11263835B2 (en) * 2017-10-27 2022-03-01 The Boeing Company Vehicle fault detection system and method utilizing graphically converted temporal data
CN110073645A (zh) * 2017-11-21 2019-07-30 深圳市尚佳能源网络有限责任公司 一种基于车牌的通讯实现方法、平台及第二终端
US10969228B2 (en) * 2018-06-05 2021-04-06 Novatel Inc. Relative position navigation system for multiple moving vehicles
US12326728B2 (en) 2019-03-22 2025-06-10 Qualcomm Incorporated System and method to control the velocity and heading of a vehicle based on preview information
US12293673B2 (en) * 2022-04-13 2025-05-06 The Boeing Company Aircraft guidance to moving target point

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Also Published As

Publication number Publication date
EP1728176A4 (en) 2012-05-30
DE04821913T1 (de) 2007-10-11
EP1728176B1 (en) 2016-01-06
US8108085B2 (en) 2012-01-31
EP1728176A1 (en) 2006-12-06
WO2005103939A1 (en) 2005-11-03
CA2555836C (en) 2013-05-28
US20110270474A1 (en) 2011-11-03
US20070021878A1 (en) 2007-01-25
CN1934562B (zh) 2010-10-06
CN1934562A (zh) 2007-03-21
CA2555836A1 (en) 2005-11-03
US8014909B2 (en) 2011-09-06

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Legal Events

Date Code Title Description
B07A Application suspended after technical examination (opinion) [chapter 7.1 patent gazette]
B09B Patent application refused [chapter 9.2 patent gazette]

Free format text: INDEFIRO O PEDIDO DE ACORDO COM ART. 8O COMBINADO COM ART. 13 E ART. 10 DA LPI

B09B Patent application refused [chapter 9.2 patent gazette]

Free format text: MANTIDO O INDEFERIMENTO UMA VEZ QUE NAO FOI APRESENTADO RECURSO DENTRO DO PRAZO LEGAL.