IT202000000331A1 - Metodo e sistema per stimare angoli aerodinamici di un corpo volante - Google Patents

Metodo e sistema per stimare angoli aerodinamici di un corpo volante

Info

Publication number
IT202000000331A1
IT202000000331A1 IT102020000000331A IT202000000331A IT202000000331A1 IT 202000000331 A1 IT202000000331 A1 IT 202000000331A1 IT 102020000000331 A IT102020000000331 A IT 102020000000331A IT 202000000331 A IT202000000331 A IT 202000000331A IT 202000000331 A1 IT202000000331 A1 IT 202000000331A1
Authority
IT
Italy
Prior art keywords
flying body
aerodynamic angles
estimating
estimating aerodynamic
angles
Prior art date
Application number
IT102020000000331A
Other languages
English (en)
Inventor
Alberto Brandl
Piero Gili
Angelo Lerro
Original Assignee
Torino Politecnico
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 Torino Politecnico filed Critical Torino Politecnico
Priority to IT102020000000331A priority Critical patent/IT202000000331A1/it
Priority to US17/777,082 priority patent/US20230003758A1/en
Priority to EP21700091.8A priority patent/EP4088121A1/en
Priority to PCT/IB2021/050157 priority patent/WO2021140491A1/en
Publication of IT202000000331A1 publication Critical patent/IT202000000331A1/it

Links

Classifications

    • 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
    • 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
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01P—MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION, OR SHOCK; INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT
    • G01P15/00—Measuring acceleration; Measuring deceleration; Measuring shock, i.e. sudden change of acceleration
    • G01P15/14—Measuring acceleration; Measuring deceleration; Measuring shock, i.e. sudden change of acceleration by making use of gyroscopes
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01P—MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION, OR SHOCK; INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT
    • G01P15/00—Measuring acceleration; Measuring deceleration; Measuring shock, i.e. sudden change of acceleration
    • G01P15/18—Measuring acceleration; Measuring deceleration; Measuring shock, i.e. sudden change of acceleration in two or more dimensions
    • 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

Landscapes

  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mathematical Optimization (AREA)
  • Mathematical Analysis (AREA)
  • Algebra (AREA)
  • Mathematical Physics (AREA)
  • Pure & Applied Mathematics (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Automation & Control Theory (AREA)
  • Navigation (AREA)
IT102020000000331A 2020-01-10 2020-01-10 Metodo e sistema per stimare angoli aerodinamici di un corpo volante IT202000000331A1 (it)

Priority Applications (4)

Application Number Priority Date Filing Date Title
IT102020000000331A IT202000000331A1 (it) 2020-01-10 2020-01-10 Metodo e sistema per stimare angoli aerodinamici di un corpo volante
US17/777,082 US20230003758A1 (en) 2020-01-10 2021-01-11 Method and system for estimating aerodynamic angles of a flying body
EP21700091.8A EP4088121A1 (en) 2020-01-10 2021-01-11 Method and system for estimating aerodynamic angles of a flying body
PCT/IB2021/050157 WO2021140491A1 (en) 2020-01-10 2021-01-11 Method and system for estimating aerodynamic angles of a flying body

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
IT102020000000331A IT202000000331A1 (it) 2020-01-10 2020-01-10 Metodo e sistema per stimare angoli aerodinamici di un corpo volante

Publications (1)

Publication Number Publication Date
IT202000000331A1 true IT202000000331A1 (it) 2021-07-10

Family

ID=70295711

Family Applications (1)

Application Number Title Priority Date Filing Date
IT102020000000331A IT202000000331A1 (it) 2020-01-10 2020-01-10 Metodo e sistema per stimare angoli aerodinamici di un corpo volante

Country Status (4)

Country Link
US (1) US20230003758A1 (it)
EP (1) EP4088121A1 (it)
IT (1) IT202000000331A1 (it)
WO (1) WO2021140491A1 (it)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN114491802A (zh) * 2022-01-11 2022-05-13 西北工业大学 基于惯组测量信息的滑翔飞行器在线气动辨识及修正方法

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1480043A1 (en) * 2003-05-13 2004-11-24 The Boeing Company Computational air data system for estimating angle-of-attack and angle-of-sideslip
WO2015008308A2 (en) 2013-07-16 2015-01-22 POLITECNICO Dl TORINO System and process for measuring and evaluating air and inertial data
RU2016142383A (ru) * 2016-10-28 2018-04-28 Акционерное общество "Научно-исследовательский институт Авиационного оборудования" Способ и устройство вычисления текущего значения углов атаки и скольжения летательного аппарата

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4046341A (en) * 1976-03-30 1977-09-06 General Electric Company Aircraft angle-of-attack and sideslip estimator

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1480043A1 (en) * 2003-05-13 2004-11-24 The Boeing Company Computational air data system for estimating angle-of-attack and angle-of-sideslip
WO2015008308A2 (en) 2013-07-16 2015-01-22 POLITECNICO Dl TORINO System and process for measuring and evaluating air and inertial data
RU2016142383A (ru) * 2016-10-28 2018-04-28 Акционерное общество "Научно-исследовательский институт Авиационного оборудования" Способ и устройство вычисления текущего значения углов атаки и скольжения летательного аппарата

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN114491802A (zh) * 2022-01-11 2022-05-13 西北工业大学 基于惯组测量信息的滑翔飞行器在线气动辨识及修正方法
CN114491802B (zh) * 2022-01-11 2024-03-29 西北工业大学 基于惯组测量信息的滑翔飞行器在线气动辨识及修正方法

Also Published As

Publication number Publication date
US20230003758A1 (en) 2023-01-05
EP4088121A1 (en) 2022-11-16
WO2021140491A1 (en) 2021-07-15

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