RU2017109733A3 - - Google Patents

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Publication number
RU2017109733A3
RU2017109733A3 RU2017109733A RU2017109733A RU2017109733A3 RU 2017109733 A3 RU2017109733 A3 RU 2017109733A3 RU 2017109733 A RU2017109733 A RU 2017109733A RU 2017109733 A RU2017109733 A RU 2017109733A RU 2017109733 A3 RU2017109733 A3 RU 2017109733A3
Authority
RU
Russia
Application number
RU2017109733A
Other languages
Russian (ru)
Other versions
RU2017109733A (ru
RU2735751C2 (ru
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 filed Critical
Publication of RU2017109733A publication Critical patent/RU2017109733A/ru
Publication of RU2017109733A3 publication Critical patent/RU2017109733A3/ru
Application granted granted Critical
Publication of RU2735751C2 publication Critical patent/RU2735751C2/ru

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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
    • 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

Landscapes

  • 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)
  • Navigation (AREA)
  • Traffic Control Systems (AREA)
RU2017109733A 2016-05-18 2017-03-23 Система адаптивной фильтрации для аэродинамических углов летательного аппарата RU2735751C2 (ru)

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
RU2017109733A RU2017109733A (ru) 2018-09-24
RU2017109733A3 true RU2017109733A3 (enExample) 2020-07-10
RU2735751C2 RU2735751C2 (ru) 2020-11-06

Family

ID=58709320

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2017109733A RU2735751C2 (ru) 2016-05-18 2017-03-23 Система адаптивной фильтрации для аэродинамических углов летательного аппарата

Country Status (6)

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

Families Citing this family (13)

* Cited by examiner, † Cited by third party
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
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
US11003196B2 (en) * 2018-12-07 2021-05-11 The Boeing Company Flight control system for determining a common mode pneumatic fault
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
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
CN115541173B (zh) * 2022-10-31 2025-12-23 厦门大学 一种绳系支撑飞机模型变速率旋转运动实现方法

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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

Also Published As

Publication number Publication date
US20170336808A1 (en) 2017-11-23
US9910445B2 (en) 2018-03-06
BR102017009774A2 (pt) 2018-03-06
RU2017109733A (ru) 2018-09-24
EP3246712A1 (en) 2017-11-22
BR102017009774B1 (pt) 2023-01-10
JP6737737B2 (ja) 2020-08-12
JP2018020759A (ja) 2018-02-08
EP3246712B1 (en) 2019-02-20
CN107436607A (zh) 2017-12-05
CN107436607B (zh) 2020-01-07
RU2735751C2 (ru) 2020-11-06

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