[go: up one dir, main page]

WO2018137004A3 - Аэрометрический способ и устройство (система) для измерений пространственного положения, рыскания и боковой скорости воздушных судов - Google Patents

Аэрометрический способ и устройство (система) для измерений пространственного положения, рыскания и боковой скорости воздушных судов Download PDF

Info

Publication number
WO2018137004A3
WO2018137004A3 PCT/AZ2018/000005 AZ2018000005W WO2018137004A3 WO 2018137004 A3 WO2018137004 A3 WO 2018137004A3 AZ 2018000005 W AZ2018000005 W AZ 2018000005W WO 2018137004 A3 WO2018137004 A3 WO 2018137004A3
Authority
WO
WIPO (PCT)
Prior art keywords
yaw
lateral velocity
air
pressures
fuselage
Prior art date
Application number
PCT/AZ2018/000005
Other languages
English (en)
French (fr)
Other versions
WO2018137004A2 (ru
Inventor
Ариф Мир Джалал оглы ПАШАЕВ
Анвер Тапдыг оглы ГАЗАРХАНОВ
Тогрул Иса оглы КАРИМЛИ
Васиф Айдын оглы НЕЙМАТОВ
Васиф Иса оглы Каримли
Original Assignee
Национальная Академия Авиации
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 Национальная Академия Авиации filed Critical Национальная Академия Авиации
Priority to EP18744734.7A priority Critical patent/EP3450989A4/en
Priority to US16/096,286 priority patent/US20190137537A1/en
Publication of WO2018137004A2 publication Critical patent/WO2018137004A2/ru
Publication of WO2018137004A3 publication Critical patent/WO2018137004A3/ru
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

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
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01P—MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION, OR SHOCK; INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT
    • G01P3/00—Measuring linear or angular speed; Measuring differences of linear or angular speeds
    • G01P3/62—Devices characterised by the determination or the variation of atmospheric pressure with height to measure the vertical components of speed
    • 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
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C5/00—Measuring height; Measuring distances transverse to line of sight; Levelling between separated points; Surveyors' levels
    • G01C5/06—Measuring height; Measuring distances transverse to line of sight; Levelling between separated points; Surveyors' levels by using barometric means
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01P—MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION, OR SHOCK; INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT
    • G01P5/00—Measuring speed of fluids, e.g. of air stream; Measuring speed of bodies relative to fluids, e.g. of ship, of aircraft
    • G01P5/14—Measuring speed of fluids, e.g. of air stream; Measuring speed of bodies relative to fluids, e.g. of ship, of aircraft by measuring differences of pressure in the fluid
    • 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
    • G05D1/04—Control of altitude or depth
    • G05D1/06—Rate of change of altitude or depth
    • G05D1/0607—Rate of change of altitude or depth specially adapted for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Automation & Control Theory (AREA)
  • Measuring Fluid Pressure (AREA)
  • Indicating Or Recording The Presence, Absence, Or Direction Of Movement (AREA)
  • Measuring Arrangements Characterized By The Use Of Fluids (AREA)

Abstract

Изобретение относится к измерительной технике для измерения пространственного положения, рыскания и боковой скорости воздушных судов. При этом используют данные от источников воздушных параметров. Определяют угол крена разностью статических давлений от приемников воздушных давлений на концевых частях крыла. Определяют угол тангажа разностью статических давлений от приемников воздушных давлений в носовой и хвостовой частях левой и правой сторонах фюзеляжа. Определяют угол рыскания и боковую скорость на основании воздушных давлений в носовой и хвостовой частях левой и правой сторонах фюзеляжа. Это достигается тем, что левосторонние и правосторонние приемники воздушных давлений, расположенные в носовой и хвостовой частях в левой и правой сторонах фюзеляжа, а также на концевых частях крыла, снабжены дополнительно горизонтально расположенными боковыми отверстиями для восприятия боковых статических воздушных давлений. При этом достигается расширение функций и технических возможностей аэрометрического способа и устройства.
PCT/AZ2018/000005 2017-01-30 2018-01-23 Аэрометрический способ и устройство (система) для измерений пространственного положения, рыскания и боковой скорости воздушных судов Ceased WO2018137004A2 (ru)

Priority Applications (2)

Application Number Priority Date Filing Date Title
EP18744734.7A EP3450989A4 (en) 2017-01-30 2018-01-23 AEROMETRIC METHOD AND DEVICE (SYSTEM) FOR MEASURING THE SPATIAL POSITION, YEAR AND SIDE SPEED OF AN AIRCRAFT
US16/096,286 US20190137537A1 (en) 2017-01-30 2018-01-23 Aerometric method and device (system) for measuring aircraft spatial position, yaw and lateral velocity

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
AZA20170019 2017-01-30
AZA20170019 2017-01-30

Publications (2)

Publication Number Publication Date
WO2018137004A2 WO2018137004A2 (ru) 2018-08-02
WO2018137004A3 true WO2018137004A3 (ru) 2018-10-25

Family

ID=62978083

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/AZ2018/000005 Ceased WO2018137004A2 (ru) 2017-01-30 2018-01-23 Аэрометрический способ и устройство (система) для измерений пространственного положения, рыскания и боковой скорости воздушных судов

Country Status (3)

Country Link
US (1) US20190137537A1 (ru)
EP (1) EP3450989A4 (ru)
WO (1) WO2018137004A2 (ru)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20190108760A1 (en) * 2017-10-10 2019-04-11 Honeywell International Inc. System and method for developing and maintaining temperature-compensated altitude information
CN111811472B (zh) * 2020-07-01 2022-03-29 亿航智能设备（广州）有限公司 一种气压计高度动态补偿方法、装置、计算机存储介质
CN112396872B (zh) * 2020-11-03 2022-04-08 海丰通航科技有限公司 一种基于计算机飞行计划cfp数据的飞机偏航判定方法、装置及存储介质
US20220355948A1 (en) * 2021-05-04 2022-11-10 The Boeing Company Computation of aircraft airspeed by inclusion of static air temperature
CN113504786B (zh) * 2021-07-08 2022-06-14 中国南方电网有限责任公司超高压输电公司大理局 一种基于风向的无人机飞行调整方法及装置
US20240265813A1 (en) * 2023-02-02 2024-08-08 Arinc Incorporated Aerodynamic instability indication of proximate uam traffic system and method

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2290646C1 (ru) * 2005-08-26 2006-12-27 Федеральное государственное унитарное предприятие "Центральный аэрогидродинамический институт им. проф. Н.Е. Жуковского" (ФГУП "ЦАГИ") Система измерения воздушных параметров полета
US7389686B2 (en) * 2006-03-22 2008-06-24 Honeywell International Inc. Methods and systems for determining air data parameters
US7770445B2 (en) * 2006-09-28 2010-08-10 Airbus France Device for wind estimation and method associated therewith
RU137952U1 (ru) * 2013-07-25 2014-02-27 Открытое акционерное общество "Ульяновское конструкторское бюро приборостроения" (ОАО "УКБП") Система измерения скорости и высоты

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2913005B2 (ja) * 1992-04-06 1999-06-28 科学技術庁航空宇宙技術研究所長 多角錐台型ピトー管型プローブを用いた飛行速度ベクトル検出システム及び多角錐台型ピトー管型プローブ
RU2157980C2 (ru) 1997-01-28 2000-10-20 Центральный аэродинамический институт им. проф. Н.Е. Жуковского Фюзеляжный приемник воздушного давления со стойкой
US6419186B1 (en) * 2000-03-31 2002-07-16 Rosemount Aerospace Inc. Standoff mounting for air data sensing probes on a helicopter
JP2005008059A (ja) * 2003-06-19 2005-01-13 Fuji Heavy Ind Ltd 自動操縦装置
JP4328660B2 (ja) * 2004-04-15 2009-09-09 富士重工業株式会社 航空機の自動離陸装置、自動着陸装置及び自動離着陸装置並びに航空機の自動離陸方法、自動着陸方法及び自動離着陸方法

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2290646C1 (ru) * 2005-08-26 2006-12-27 Федеральное государственное унитарное предприятие "Центральный аэрогидродинамический институт им. проф. Н.Е. Жуковского" (ФГУП "ЦАГИ") Система измерения воздушных параметров полета
US7389686B2 (en) * 2006-03-22 2008-06-24 Honeywell International Inc. Methods and systems for determining air data parameters
US7770445B2 (en) * 2006-09-28 2010-08-10 Airbus France Device for wind estimation and method associated therewith
RU137952U1 (ru) * 2013-07-25 2014-02-27 Открытое акционерное общество "Ульяновское конструкторское бюро приборостроения" (ОАО "УКБП") Система измерения скорости и высоты

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
See also references of EP3450989A4 *

Also Published As

Publication number Publication date
US20190137537A1 (en) 2019-05-09
EP3450989A4 (en) 2019-12-25
EP3450989A2 (en) 2019-03-06
WO2018137004A2 (ru) 2018-08-02

Similar Documents

Publication Publication Date Title
WO2018137004A3 (ru) Аэрометрический способ и устройство (система) для измерений пространственного положения, рыскания и боковой скорости воздушных судов
MX2018002742A (es) Aparatos y metodos para vehiculos aereos no tripulados con control de gestos.
GB2564325A (en) Systems and methods for autonomous drone navigation
MX2015009368A (es) Experiencia de cabina de vehiculo integrada.
EP4283340A3 (en) Navigating unmanned aircraft using pitch
WO2017087653A3 (en) Generating simulated images from design information
EP3362360A4 (en) PARATROOF CONTROL SYSTEM FOR AN UNMANUFACTURED AIRCRAFT
Lungu et al. Application of H2/H∞ and dynamic inversion techniques to aircraft landing control
MX371436B (es) Deteccion de puerta para pasajeros multiples para el transporte de pasajeros.
EP3947147A4 (en) FLIGHT CONTROL SYSTEM FOR UNMANNED AERIAL VEHICLE AND TOPOGRAPHY MEASUREMENT SYSTEM
EP2793096A3 (en) Flight system for an aircraft having an autoland system
WO2015175077A3 (en) Projected synthetic vision
WO2015195173A3 (en) Tactile and peripheral vision combined modality hover drift cueing
EP3280645A4 (en) System and method for angle of attack indication with no dedicated sensors and aircraft information
WO2015126513A3 (en) Peripheral vision hover drift cueing
WO2016018491A3 (en) Advanced aircraft vision system utilizing multi-sensor gain scheduling
BR112017020023A2 (pt) sistema de liberação de material
BR112017016025A2 (pt) dispositivo de posicionamento de componentes de aeronave, sistema de montagem de aeronave e método de montagem de aeronave
BR112018000870A2 (pt) método e sistema de controle de veículo
EP3299925A3 (en) Method, apparatus and system for controlling unmanned aerial vehicle
EP2492892A3 (en) Aircraft systems and methods for providing exhaust warnings
GB2574501B (en) Monitoring system for the cabin of an aircraft, data distribution apparatus and aircraft
CN104374541A (zh) 一种l形压力受感器的静压计算方法
EP3182240A3 (en) High authority stability and control augmentation system
EP4024368A4 (en) DELIVERY DEVICE, AIRCRAFT, FLIGHT SYSTEM, METHOD THEREFOR, AND NON-TRANSITORY COMPUTER READABLE MEDIUM

Legal Events

Date Code Title Description
WWE Wipo information: entry into national phase

Ref document number: 2018744734

Country of ref document: EP

121 Ep: the epo has been informed by wipo that ep was designated in this application

Ref document number: 18744734

Country of ref document: EP

Kind code of ref document: A2

ENP Entry into the national phase

Ref document number: 2018744734

Country of ref document: EP

Effective date: 20181127

NENP Non-entry into the national phase

Ref country code: DE