CN105988480B - 飞行控制系统命令选择和数据传输 - Google Patents

飞行控制系统命令选择和数据传输 Download PDF

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Publication number
CN105988480B
CN105988480B CN201610163767.5A CN201610163767A CN105988480B CN 105988480 B CN105988480 B CN 105988480B CN 201610163767 A CN201610163767 A CN 201610163767A CN 105988480 B CN105988480 B CN 105988480B
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China
Prior art keywords
actuator
commands
command
backup
control command
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CN201610163767.5A
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Chinese (zh)
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CN105988480A (zh
Inventor
G·松井
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Boeing Co
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Boeing Co
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Publication of CN105988480A publication Critical patent/CN105988480A/zh
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    • 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
    • B64C13/24—Transmitting means
    • B64C13/38—Transmitting means with power amplification
    • B64C13/50—Transmitting means with power amplification using electrical energy
    • B64C13/505—Transmitting means with power amplification using electrical energy having duplication or stand-by provisions
    • 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
    • G05D1/101—Simultaneous control of position or course in three dimensions specially adapted for aircraft
    • G—PHYSICS
    • G06—COMPUTING OR CALCULATING; COUNTING
    • G06F—ELECTRIC DIGITAL DATA PROCESSING
    • G06F11/00—Error detection; Error correction; Monitoring
    • G06F11/07—Responding to the occurrence of a fault, e.g. fault tolerance
    • G06F11/08—Error detection or correction by redundancy in data representation, e.g. by using checking codes
    • G06F11/10—Adding special bits or symbols to the coded information, e.g. parity check, casting out 9's or 11's
    • G06F11/1004—Adding special bits or symbols to the coded information, e.g. parity check, casting out 9's or 11's to protect a block of data words, e.g. CRC or checksum

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  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Theoretical Computer Science (AREA)
  • Automation & Control Theory (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Computer Security & Cryptography (AREA)
  • Quality & Reliability (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Control Of Driving Devices And Active Controlling Of Vehicle (AREA)
  • Testing And Monitoring For Control Systems (AREA)
  • Safety Devices In Control Systems (AREA)
  • Programmable Controllers (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
CN201610163767.5A 2015-03-20 2016-03-18 飞行控制系统命令选择和数据传输 Active CN105988480B (zh)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US14/664,355 2015-03-20
US14/664,355 US9493231B2 (en) 2015-03-20 2015-03-20 Flight control system command selection and data transport

Publications (2)

Publication Number Publication Date
CN105988480A CN105988480A (zh) 2016-10-05
CN105988480B true CN105988480B (zh) 2021-02-23

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CN201610163767.5A Active CN105988480B (zh) 2015-03-20 2016-03-18 飞行控制系统命令选择和数据传输

Country Status (6)

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US (1) US9493231B2 (enExample)
EP (1) EP3079063B1 (enExample)
JP (1) JP6587561B2 (enExample)
CN (1) CN105988480B (enExample)
BR (1) BR102016004145B1 (enExample)
CA (1) CA2918108C (enExample)

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US10248430B2 (en) 2016-12-16 2019-04-02 Hamilton Sundstrand Corporation Runtime reconfigurable dissimilar processing platform
WO2018142246A1 (en) * 2017-02-01 2018-08-09 Thales Canada Inc. Backup actuation control unit for controlling an actuator dedicated to a given surface and method of using same
US10336437B2 (en) * 2017-05-05 2019-07-02 Hamilton Sundstrand Corporation Method to measure aircraft high-lift system brake response time
US10571914B2 (en) * 2017-06-29 2020-02-25 The Boeing Company Fault coverage for multiple failures in redundant systems
US10353767B2 (en) * 2017-09-14 2019-07-16 Bae Systems Controls Inc. Use of multicore processor to mitigate common mode computing faults
TR201716275A1 (tr) * 2017-10-23 2019-05-21 Tuerkiye Bilimsel Ve Teknolojik Arastirma Kurumu Tuebitak Hava araçlari i̇çi̇n bi̇r kontrol paneli̇ denetleme ci̇hazi
US11131991B2 (en) * 2018-01-19 2021-09-28 Ge Aviation Systems Llc Autopilot control system for unmanned vehicles
US10988237B1 (en) * 2019-12-17 2021-04-27 The Boeing Company Feed forward equalization control for active-active redundant actuation systems
EP3862835B1 (en) * 2020-02-10 2023-10-25 Volocopter GmbH Method and system for monitoring a condition of a vtol-aircraft
US11155356B2 (en) * 2020-02-19 2021-10-26 Kitty Hawk Corporation Thrust allocation using optimization in a distributed flight control system
CN116243594B (zh) * 2023-05-11 2023-08-04 广州汽车集团股份有限公司 一种飞行器控制系统、飞行控制方法、存储介质

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101142122A (zh) * 2005-03-18 2008-03-12 雅马哈发动机株式会社 飞行控制系统

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US7167452B2 (en) * 2002-07-23 2007-01-23 Lockheed Martin Corporation Selection of data to be transmitted between nodes in a network having limited bandwidth
WO2007018651A1 (en) * 2005-08-05 2007-02-15 Honeywell International, Inc. Method for redunancy management of distributed and recoverable digital control system
WO2007094808A1 (en) * 2005-08-05 2007-08-23 Honeywell International Inc. Monitoring system and methods for a distributed and recoverable digital control system
US7421320B2 (en) * 2005-10-06 2008-09-02 The Boeing Company Methods and apparatus for implementing mid-value selection functions for dual dissimlar processing modules
EP1977292A2 (en) * 2006-01-17 2008-10-08 Gulfstream Aerospace Corporation System and method for an integrated backup control system
CA2637226A1 (en) * 2006-01-17 2007-07-26 Gulfstream Aerospace Corporation Apparatus and method for backup control in a distributed flight control system
US7693616B2 (en) * 2006-03-31 2010-04-06 Honeywell International Inc. System and method of redundancy management for fault effect mitigation
US8386093B2 (en) * 2007-04-05 2013-02-26 Bombardier Inc. Multi-axis serially redundant, single channel, multi-path fly-by-wire flight control system
US7840316B2 (en) * 2007-12-17 2010-11-23 Honeywell International Inc. Limited authority and full authority mode fly-by-wire flight control surface actuation control system
FR2927308B1 (fr) * 2008-02-08 2010-10-22 Airbus France Systeme distribue de commande de vol.
FR2941912B1 (fr) * 2009-02-10 2011-02-18 Airbus France Systeme de commande de vol et aeronef le comportant
FR2959835B1 (fr) * 2010-05-10 2012-06-15 Airbus Operations Sas Systeme de commande de vol et aeronef le comportant
US8601150B1 (en) * 2010-10-01 2013-12-03 The Boeing Company Cross-channel data link

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101142122A (zh) * 2005-03-18 2008-03-12 雅马哈发动机株式会社 飞行控制系统

Also Published As

Publication number Publication date
CA2918108A1 (en) 2016-09-20
BR102016004145A2 (pt) 2016-09-20
EP3079063A2 (en) 2016-10-12
JP6587561B2 (ja) 2019-10-09
CA2918108C (en) 2020-03-24
US9493231B2 (en) 2016-11-15
JP2016210407A (ja) 2016-12-15
BR102016004145B1 (pt) 2022-08-16
US20160272300A1 (en) 2016-09-22
EP3079063B1 (en) 2020-05-06
EP3079063A3 (en) 2016-11-16
CN105988480A (zh) 2016-10-05

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