BRPI0517266A - sistema de controle de vÈo que tem um projeto de laço de controle triplo - Google Patents

sistema de controle de vÈo que tem um projeto de laço de controle triplo

Info

Publication number
BRPI0517266A
BRPI0517266A BRPI0517266-7A BRPI0517266A BRPI0517266A BR PI0517266 A BRPI0517266 A BR PI0517266A BR PI0517266 A BRPI0517266 A BR PI0517266A BR PI0517266 A BRPI0517266 A BR PI0517266A
Authority
BR
Brazil
Prior art keywords
triple
control system
control
flight
design
Prior art date
Application number
BRPI0517266-7A
Other languages
English (en)
Inventor
Jack Shyhpyng Shue
John J Schillings
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
Application filed by Bell Helicopter Textron Inc filed Critical Bell Helicopter Textron Inc
Publication of BRPI0517266A publication Critical patent/BRPI0517266A/pt

Links

Classifications

    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot
    • G05D1/10—Simultaneous control of position or course in three dimensions
    • G05D1/101—Simultaneous control of position or course in three dimensions specially adapted for aircraft

Abstract

SISTEMA DE CONTROLE DE VÈO QUE TEM UM PROJETO DE LAçO DE CONTROLE TRIPLO. Trata-se de um sistema de controle de vóo que é configurado para controlar o vóo de uma aeronave utilizando um projeto de controle de laço triplo para aumentar solidamente o desempenho do sistema. Um laço interno compreende um melhor método de busca de Regulador quadrático linear (LQR), e um laço externo compreende uma realimentação clássica de projeto de ganho sumário. Um terceiro laço compreende um método de busca de compensação em estado estacionário.
BRPI0517266-7A 2004-11-08 2005-11-08 sistema de controle de vÈo que tem um projeto de laço de controle triplo BRPI0517266A (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US62584804P 2004-11-08 2004-11-08
PCT/US2005/040394 WO2007018572A2 (en) 2004-11-08 2005-11-08 Flight system with three feedback control loops

Publications (1)

Publication Number Publication Date
BRPI0517266A true BRPI0517266A (pt) 2008-10-07

Family

ID=37727758

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0517266-7A BRPI0517266A (pt) 2004-11-08 2005-11-08 sistema de controle de vÈo que tem um projeto de laço de controle triplo

Country Status (7)

Country Link
US (1) US8473124B2 (pt)
EP (1) EP1810099B1 (pt)
CN (1) CN100591900C (pt)
BR (1) BRPI0517266A (pt)
CA (1) CA2585105C (pt)
DE (1) DE05858477T1 (pt)
WO (1) WO2007018572A2 (pt)

Families Citing this family (60)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7930074B2 (en) * 2007-03-19 2011-04-19 Sikorsky Aircraft Corporation Vertical speed and flight path command module for displacement collective utilizing tactile cueing and tactile feedback
US8694182B2 (en) * 2007-04-03 2014-04-08 Sikorsky Aircraft Corporation Altitude and acceleration command altitude hold algorithm for rotorcraft with large center of gravity range
FR2924505B1 (fr) * 2007-12-04 2015-12-11 Thales Sa Methode de decouplage du mode de suivi automatique du profil lateral et du mode de suivi automatique du profil vertical
FR2935495B1 (fr) * 2008-08-29 2010-09-10 Thales Sa Systeme et procede de calcul des predictions de vol par sections verticales
EP2342609B1 (en) * 2008-10-03 2015-03-04 Bell Helicopter Textron Inc. Method and apparatus for aircraft sensor and actuator failure protection using reconfigurable flight control laws
US8529189B2 (en) * 2009-01-30 2013-09-10 Honeywell International Inc. Linear quadratic regulator control for bleed air system fan air valve
DE202009001355U1 (de) 2009-02-04 2009-05-20 RÖHR, Ulrich Modellflugkörpersteuer- und Empfangseinrichtung
US8718839B2 (en) * 2009-12-06 2014-05-06 Evolved Aircraft Systems, L.L.C. Method and apparatus for automatically controlling aircraft flight control trim systems
CA2784615C (en) * 2009-12-18 2017-03-28 National Research Council Of Canada Response mode for control system of piloted craft
KR101184625B1 (ko) 2010-04-15 2012-09-21 국방과학연구소 비행체의 수직면 직선추종 비행 제어기 설계방법
US8965538B2 (en) * 2010-05-19 2015-02-24 The Boeing Company Methods and apparatus for state limiting in a control system
CN102023640B (zh) * 2010-11-23 2012-07-04 北京航空航天大学 飞行包线内标称设计点的选择方法
ITRM20110651A1 (it) * 2010-12-20 2012-06-21 Selex Sistemi Integrati Spa Metodo di previsione rapida del profilo verticale della traiettoria per la gestione del traffico aereo, e relativo sistema atm.
EP2635942B1 (en) * 2011-01-14 2015-06-17 Bell Helicopter Textron Inc. Flight control laws for vertical flight path control
WO2012134460A1 (en) * 2011-03-30 2012-10-04 Bell Helicopter Textron Inc. Flight control laws for constant vector flat turns
DE102012003910A1 (de) 2011-04-15 2012-10-18 Ulrich Röhr System zur drahtlosen Steuerung eines RC-Modells, Sendeeinrichtung, Empfangseinrichtung sowie Verfahren
CA2974171C (en) * 2011-07-15 2019-11-12 Bell Helicopter Textron Inc. Flight control laws for automatic hover hold
TW201307155A (zh) * 2011-08-01 2013-02-16 Hon Hai Prec Ind Co Ltd 無人飛行載具模擬飛行系統及方法
CN102566427A (zh) * 2012-01-09 2012-07-11 南京航空航天大学 一种飞行器鲁棒控制方法
US9150308B2 (en) * 2012-02-10 2015-10-06 Merlin Technology, Inc. Rotorcraft autopilot system, components and methods
US9097529B2 (en) * 2012-07-12 2015-08-04 Honeywell International Inc. Aircraft system and method for improving navigation performance
JP6267700B2 (ja) * 2012-07-18 2018-01-24 クレアフォーム・インコーポレイテッドＣｒｅａｆｏｒｍ Ｉｎｃ． ３ｄ走査および位置決めのインターフェース
CN102929150B (zh) * 2012-11-13 2015-02-11 湖南航天机电设备与特种材料研究所 一种基于离散控制模型的扰流片自适应控制方法
US10421531B2 (en) * 2012-11-27 2019-09-24 Bell Helicopter Textron Inc. Laptop based rapid control laws development
KR101426289B1 (ko) * 2013-01-09 2014-08-05 국방과학연구소 기동 헬기 측면 항법 운용 장치
KR101434310B1 (ko) 2013-05-22 2014-08-26 현대로템 주식회사 이동장비에 장착된 구동장치의 안정화성능 향상 기법 및 시스템과 그 이동장비
US9856017B2 (en) * 2013-06-11 2018-01-02 Bell Helicopter Textron Inc. Torque based method of limiting vertical axis augmentation
JP5698802B2 (ja) * 2013-06-28 2015-04-08 ヤマハ発動機株式会社 遠隔操縦装置
CN103823380B (zh) * 2014-03-14 2017-01-18 北京航空航天大学 一种考虑飞行品质的直升机总体设计方法
US9429952B2 (en) * 2014-04-04 2016-08-30 Sikorsky Aircraft Corporation Rotorcraft control laws for sea-based operations
CN104298109B (zh) * 2014-09-23 2017-04-19 南京航空航天大学 基于多控制器融合的无尾飞行器协调转弯控制方法
WO2016054209A1 (en) 2014-10-01 2016-04-07 Sikorsky Aircraft Corporation Dual rotor, rotary wing aircraft
US20170267338A1 (en) 2014-10-01 2017-09-21 Sikorsky Aircraft Corporation Acoustic signature variation of aircraft utilizing a clutch
WO2016178738A1 (en) * 2015-05-05 2016-11-10 Sikorsky Aircraft Corporation Position hold override control
US10633092B2 (en) 2015-12-07 2020-04-28 Aai Corporation UAV with wing-plate assemblies providing efficient vertical takeoff and landing capability
CN105867399B (zh) * 2016-04-18 2017-05-03 北京航天自动控制研究所 一种确定多状态跟踪制导参数的方法
WO2018213872A1 (en) 2017-05-22 2018-11-29 The Bionics Institute Of Australia "systems and methods for monitoring neural activity"
JP7111710B2 (ja) 2016-08-08 2022-08-02 ディープ・ブレイン・スティムレーション・テクノロジーズ・ピーティーワイ・リミテッド 神経活動をモニタするためのシステム及び方法
CN106546204B (zh) * 2016-09-22 2018-12-18 北京空间飞行器总体设计部 一种舱间分离相对位置与姿态测量方法
CN108008630B (zh) * 2016-11-01 2022-04-19 贵州火星探索科技有限公司 一种无人机位置环的补偿器设计方法及装置
US10654561B2 (en) * 2017-02-02 2020-05-19 Textron Innovations Inc. Rotorcraft fly-by-wire go-around mode
US10287026B2 (en) 2017-02-04 2019-05-14 Bell Helicopter Textron Inc. Power demand anticipation systems for rotorcraft
US10647414B2 (en) * 2017-02-27 2020-05-12 Textron Innovations Inc. Rotorcraft fly-by-wire standard rate turn
US10093415B1 (en) * 2017-03-20 2018-10-09 Bell Helicopter Textron Inc. System and method for rotorcraft heading control
CA2972498C (en) * 2017-06-28 2024-01-23 Bombardier Inc. Takeoff pitch guidance system and method
JP2019113992A (ja) * 2017-12-22 2019-07-11 カシオ計算機株式会社 飛行装置、飛行装置の制御方法及びプログラム
CN109032171B (zh) * 2018-06-26 2019-07-16 中国空气动力研究与发展中心低速空气动力研究所 一种基于非线性控制律的飞行器风洞自由飞的控制方法
CN109765530B (zh) * 2018-12-30 2021-02-19 成都汇蓉国科微系统技术有限公司 一种运动平台雷达波束解耦方法
US11059577B2 (en) * 2019-03-25 2021-07-13 Textron Innovations Inc. System and method for monitoring aircraft pilot control position and providing a retrim prompt
CN110187715B (zh) * 2019-04-24 2021-01-15 南京航空航天大学 一种基于动态耦合分析的高超声速飞行器协调控制方法
CN110221624B (zh) * 2019-05-20 2021-08-17 南京航空航天大学 一种基于组合系统的无人机环绕地面目标制导方法
CN110568758B (zh) * 2019-09-12 2022-07-01 中汽研（天津）汽车工程研究院有限公司 一种自动驾驶汽车的参数自适应横向运动lqr控制方法
EP3832424B1 (en) 2019-12-02 2022-07-13 Volocopter GmbH Method of operating an actuator system, actuator system, and aircraft comprising said method and system
CN111026160B (zh) * 2019-12-26 2020-12-08 华中科技大学 一种四旋翼无人机轨迹跟踪控制方法
CN111290420A (zh) * 2020-03-11 2020-06-16 山东超越数控电子股份有限公司 飞行器飞行姿态控制系统和方法
CN112286053B (zh) * 2020-10-16 2021-08-27 北京航空航天大学 一种高机动微型无人机的制导控制一体化方法
CN112379685B (zh) * 2020-11-30 2022-02-11 中国科学院沈阳自动化研究所 一种基于风速风向传感器的旋翼无人机控制系统及方法
US11592837B1 (en) 2021-10-30 2023-02-28 Beta Air, Llc Systems and methods to control gain for an electric aircraft
CN114995140B (zh) * 2022-06-07 2023-01-24 哈尔滨工业大学 一种基于直/气复合的高超声速飞行器时变系统的控制方法
CN115328185B (zh) * 2022-08-30 2023-05-30 北京京航计算通讯研究所 一种飞行器非线性非定常气动载荷修正系统

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4466526A (en) * 1982-04-16 1984-08-21 Chandler Evans Inc. Helicopter engine control with rotor speed decay anticipator
US5189620A (en) * 1989-10-06 1993-02-23 United Technologies Corporation Control system for gas turbine helicopter engines and the like
US6539290B1 (en) * 1995-06-07 2003-03-25 Dabulamanzi Holdings, Llc Method, apparatus and design procedure for controlling multi-input, multi-output (MIMO) parameter dependent systems using feedback LTI'zation
US5796922A (en) * 1996-03-29 1998-08-18 Weber State University Trainable, state-sampled, network controller
AU6532698A (en) * 1996-12-05 1998-06-29 Shabbir Ahmed Parvez Autonomous on-board orbit control/maintenance system for satellites
US6729139B2 (en) * 2001-09-26 2004-05-04 Goodrich Pump & Engine Control Systems, Inc. Engine control system
GB2423377B (en) * 2002-12-09 2007-04-18 Georgia Tech Res Inst Adaptive Output Feedback Apparatuses And Methods Capable Of Controlling A Non-Minimum Phase System
US7343232B2 (en) * 2003-06-20 2008-03-11 Geneva Aerospace Vehicle control system including related methods and components

Also Published As

Publication number Publication date
WO2007018572A2 (en) 2007-02-15
EP1810099B1 (en) 2016-09-07
EP1810099A4 (en) 2008-03-12
DE05858477T1 (de) 2008-01-31
WO2007018572A9 (en) 2008-04-03
CN100591900C (zh) 2010-02-24
CN101175909A (zh) 2008-05-07
WO2007018572A3 (en) 2007-11-29
US20080097658A1 (en) 2008-04-24
CA2585105C (en) 2015-04-21
EP1810099A2 (en) 2007-07-25
CA2585105A1 (en) 2007-02-15
US8473124B2 (en) 2013-06-25

Similar Documents

Publication Publication Date Title
BRPI0517266A (pt) sistema de controle de vÈo que tem um projeto de laço de controle triplo
BRPI0519214A2 (pt) sistema e mÉtodo de controle de vâo e aeronave
BRPI0508489A (pt) efeitos de instabilidade de controle
BR102016003475A8 (pt) Método para regulação de fluxo de corrente cruzada
BRPI0518298A2 (pt) disposiÇço para a reduÇço do ruÍdo aerodinÂmico em uma asa auxiliar de um aviço
GB2396706A (en) Airplane emergency navigational system
AU2018203153A1 (en) Systems and methods for acoustic radiation control
BR112017027689A2 (pt) regulador de tensão de baixa queda, método para melhorar a estabilidade do regulador de tensão de baixa queda e malha de captura de fase
BR112015029803A2 (pt) método e aparato para estabilizar pressão em um conjunto regulador inteligente
ATE544673T1 (de) Klappbarer kantenzaun einer hinterkantklappe und betriebsverfahren
WO2007011408A3 (en) High-lift distributed active flow control system and method
BR112014008198A2 (pt) válvula de controle sanguíneo de múltiplo uso contendo frestas circunferênciais
BR112016002181A2 (pt) controle de um modo de acesso atual de um dispositivo de computação com base em um estado de um mecanismo de fixação
FR2955309B1 (fr) Systeme de commande de vol pour un aeronef
BR112015017917A2 (pt) arquitetura para suprir potência elétrica de emergência para uma aeronave, aeronave e método para suprir potência elétrica de emergência em uma aeronave
BR112016014950A2 (pt) Módulo de membrana de fibra oca
BR112014019373A8 (pt) Formulação agroquímica, e, método de fabricação de uma formulação
BR112022002171A2 (pt) Composto bis-amida e uso do mesmo
BR112022021714A2 (pt) Controle de amplificador de potência com uma matriz de antenas
BR112016027730A8 (pt) processo para controlar empuxo de marcha lenta de um turbojato, meio de dados legível por computador, dispositivo de controle, e, turbojato
BR112014010587A2 (pt) biocontrole de nematódeos
BRPI0516730A (pt) sistema de assistência de energia auxiliar de controle de vÈo mecánico
BR112017016286A2 (pt) ?sistema de controle, barra de pulverização, veículo e método para implementar um sistema de controle?
BR112014008521A2 (pt) sistema de lâmpada de despertar
BR112013028684A2 (pt) dispositivo que provê alarme de despertar, programa de computador, e, método para prover um sinal de despertar audível durante um período de alerta

Legal Events

Date Code Title Description
B08F Application dismissed because of non-payment of annual fees [chapter 8.6 patent gazette]

Free format text: REFERENTE A 10A ANUIDADE.

B08K Patent lapsed as no evidence of payment of the annual fee has been furnished to inpi [chapter 8.11 patent gazette]

Free format text: EM VIRTUDE DO ARQUIVAMENTO PUBLICADO NA RPI 2343 DE 01-12-2015 E CONSIDERANDO AUSENCIA DE MANIFESTACAO DENTRO DOS PRAZOS LEGAIS, INFORMO QUE CABE SER MANTIDO O ARQUIVAMENTO DO PEDIDO DE PATENTE, CONFORME O DISPOSTO NO ARTIGO 12, DA RESOLUCAO 113/2013.