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 PDFInfo
- 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
Links
- 239000000523 sample Substances 0.000 abstract 3
- 230000003068 static effect Effects 0.000 abstract 3
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)
- Measuring Arrangements Characterized By The Use Of Fluids (AREA)
- Indicating Or Recording The Presence, Absence, Or Direction Of Movement (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.
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 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 (4)
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 |
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 |
Citations (4)
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)
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 |
-
2018
- 2018-01-23 US US16/096,286 patent/US20190137537A1/en not_active Abandoned
- 2018-01-23 WO PCT/AZ2018/000005 patent/WO2018137004A2/ru active Application Filing
- 2018-01-23 EP EP18744734.7A patent/EP3450989A4/en not_active Withdrawn
Patent Citations (4)
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)
Title |
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See also references of EP3450989A4 * |
Also Published As
Publication number | Publication date |
---|---|
US20190137537A1 (en) | 2019-05-09 |
EP3450989A2 (en) | 2019-03-06 |
EP3450989A4 (en) | 2019-12-25 |
WO2018137004A2 (ru) | 2018-08-02 |
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