JP6737737B2 - 航空機の空力角度のための適合フィルタリングシステム - Google Patents

航空機の空力角度のための適合フィルタリングシステム Download PDF

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JP6737737B2
JP6737737B2 JP2017089267A JP2017089267A JP6737737B2 JP 6737737 B2 JP6737737 B2 JP 6737737B2 JP 2017089267 A JP2017089267 A JP 2017089267A JP 2017089267 A JP2017089267 A JP 2017089267A JP 6737737 B2 JP6737737 B2 JP 6737737B2
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angle
aerodynamic angle
inertial
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JP2018020759A5 (enExample
JP2018020759A (ja
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ジャ ルオ，
ジャ ルオ，
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Boeing Co
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Boeing Co
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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
    • 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
    • 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
    • G05D1/0816—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft to ensure stability
    • G05D1/0825—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft to ensure stability using mathematical models
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01P—MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION, OR SHOCK; INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT
    • G01P13/00—Indicating or recording presence, absence, or direction, of movement
    • G01P13/02—Indicating direction only, e.g. by weather vane
    • G01P13/025—Indicating direction only, e.g. by weather vane indicating air data, i.e. flight variables of an aircraft, e.g. angle of attack, side slip, shear, yaw
    • 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
    • B64C13/18—Initiating means actuated automatically, e.g. responsive to gust detectors using automatic pilot
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D43/00—Arrangements or adaptations of instruments
    • B64D43/02—Arrangements or adaptations of instruments for indicating aircraft speed or stalling conditions
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D47/00—Equipment not otherwise provided for
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05B—CONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
    • G05B13/00—Adaptive control systems, i.e. systems automatically adjusting themselves to have a performance which is optimum according to some preassigned criterion
    • 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
    • G—PHYSICS
    • G06—COMPUTING OR CALCULATING; COUNTING
    • G06F—ELECTRIC DIGITAL DATA PROCESSING
    • G06F17/00—Digital computing or data processing equipment or methods, specially adapted for specific functions
    • G06F17/40—Data acquisition and logging
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U10/00—Type of UAV
    • B64U10/25—Fixed-wing aircraft

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  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Automation & Control Theory (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Mathematical Physics (AREA)
  • Pure & Applied Mathematics (AREA)
  • Mathematical Optimization (AREA)
  • Mathematical Analysis (AREA)
  • Algebra (AREA)
  • General Engineering & Computer Science (AREA)
  • Theoretical Computer Science (AREA)
  • Software Systems (AREA)
  • Health & Medical Sciences (AREA)
  • Artificial Intelligence (AREA)
  • Computer Vision & Pattern Recognition (AREA)
  • Evolutionary Computation (AREA)
  • Medical Informatics (AREA)
  • Databases & Information Systems (AREA)
  • Data Mining & Analysis (AREA)
  • Computer Hardware Design (AREA)
  • Traffic Control Systems (AREA)
  • Navigation (AREA)
JP2017089267A 2016-05-18 2017-04-28 航空機の空力角度のための適合フィルタリングシステム Active JP6737737B2 (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US15/157,762 2016-05-18
US15/157,762 US9910445B2 (en) 2016-05-18 2016-05-18 Adaptive filtering system for aerodynamic angles of an aircraft

Publications (3)

Publication Number Publication Date
JP2018020759A JP2018020759A (ja) 2018-02-08
JP2018020759A5 JP2018020759A5 (enExample) 2020-06-25
JP6737737B2 true JP6737737B2 (ja) 2020-08-12

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JP2017089267A Active JP6737737B2 (ja) 2016-05-18 2017-04-28 航空機の空力角度のための適合フィルタリングシステム

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US (1) US9910445B2 (enExample)
EP (1) EP3246712B1 (enExample)
JP (1) JP6737737B2 (enExample)
CN (1) CN107436607B (enExample)
BR (1) BR102017009774B1 (enExample)
RU (1) RU2735751C2 (enExample)

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Publication number Priority date Publication date Assignee Title
US20190217966A1 (en) * 2018-01-12 2019-07-18 Rosemount Aerospace Inc. Aircraft air data generation using laser sensor data and inertial sensor data
US11066189B2 (en) 2018-12-07 2021-07-20 The Boeing Company Flight control system for determining estimated dynamic pressure based on lift and drag coefficients
US11003196B2 (en) * 2018-12-07 2021-05-11 The Boeing Company Flight control system for determining a common mode pneumatic fault
US11029706B2 (en) 2018-12-07 2021-06-08 The Boeing Company Flight control system for determining a fault based on error between a measured and an estimated angle of attack
US11186357B2 (en) * 2019-01-03 2021-11-30 Textron Innovations Inc. System and method for controlling rotorcraft
US12123894B2 (en) 2019-05-01 2024-10-22 Queen's University At Kingston Apparatus and method for measuring velocity perturbations in a fluid
USD902829S1 (en) * 2019-07-15 2020-11-24 Darold B Cummings Aircraft
USD941741S1 (en) * 2019-08-23 2022-01-25 Darold B Cummings Aircraft
JP7265260B2 (ja) * 2019-09-17 2023-04-26 国立研究開発法人宇宙航空研究開発機構 航空機
US12379730B2 (en) 2021-03-31 2025-08-05 Beta Air Llc Methods and systems for flight control configured for use in an electric aircraft
WO2023044173A2 (en) * 2021-09-17 2023-03-23 Beta Air, Llc Methods and systems for flight control configured for use in an electric aircraft
CN114878856B (zh) * 2022-04-15 2025-09-19 中国航空工业集团公司沈阳飞机设计研究所 一种表决后的真攻角与侧滑角滤波方法及系统

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US5170969A (en) * 1988-11-23 1992-12-15 The Boeing Company Aircraft rudder command system
US5669582A (en) 1995-05-12 1997-09-23 The Boeing Company Method and apparatus for reducing unwanted sideways motion in the aft cabin and roll-yaw upsets of an airplane due to atmospheric turbulence and wind gusts
US6273370B1 (en) 1999-11-01 2001-08-14 Lockheed Martin Corporation Method and system for estimation and correction of angle-of-attack and sideslip angle from acceleration measurements
US6711476B2 (en) * 2001-09-27 2004-03-23 The Boeing Company Method and computer program product for estimating at least one state of a dynamic system
US6928341B2 (en) * 2003-05-13 2005-08-09 The Boeing Company Computational air data system for angle-of-attack and angle-of-sideslip
EP2615026B1 (en) * 2011-06-10 2018-04-04 Airbus Defence and Space GmbH Method and apparatus for minimizing dynamic structural loads of an aircraft
FR2978858B1 (fr) * 2011-08-01 2013-08-30 Airbus Operations Sas Procede et systeme pour la determination de parametres de vol d'un aeronef
US9498903B2 (en) * 2012-10-31 2016-11-22 The Boeing Company System and method for manufacturing monolithic structures using expanding internal tools
RU2541902C2 (ru) * 2013-04-29 2015-02-20 Открытое акционерное общество "Лётно-исследовательский институт имени М.М. Громова" Интеллектуальная система поддержки экипажа
CN103926837B (zh) * 2014-04-22 2016-05-25 西北工业大学 多种耦合作用下飞行器综合解耦方法
CN103914074A (zh) * 2014-04-22 2014-07-09 西北工业大学 飞行器推力强耦合解耦方法
RU159568U1 (ru) * 2015-06-15 2016-02-10 Акционерное общество "Ульяновское конструкторское бюро приборостроения" (АО "УКБП") Система предупреждения критических режимов для маневренных самолетов

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Publication number Publication date
US9910445B2 (en) 2018-03-06
JP2018020759A (ja) 2018-02-08
BR102017009774A2 (pt) 2018-03-06
EP3246712B1 (en) 2019-02-20
RU2017109733A3 (enExample) 2020-07-10
RU2017109733A (ru) 2018-09-24
US20170336808A1 (en) 2017-11-23
RU2735751C2 (ru) 2020-11-06
EP3246712A1 (en) 2017-11-22
CN107436607B (zh) 2020-01-07
CN107436607A (zh) 2017-12-05
BR102017009774B1 (pt) 2023-01-10

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