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List of aerospace equivalent terms -- Part 4: Flight dynamics
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GB/T 35853.4-2018
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Basic data | Standard ID | GB/T 35853.4-2018 (GB/T35853.4-2018) | | Description (Translated English) | List of aerospace equivalent terms -- Part 4: Flight dynamics | | Sector / Industry | National Standard (Recommended) | | Classification of Chinese Standard | V36 | | Classification of International Standard | 49.020 | | Word Count Estimation | 36,363 | | Date of Issue | 2018-03-15 | | Date of Implementation | 2018-10-01 | | Adopted Standard | ISO 5843-4-1990, MOD | | Regulation (derived from) | National Standards Announcement No. 3 of 2018 | | Issuing agency(ies) | State Administration for Market Regulation, China National Standardization Administration | | Summary | This standard specifies the terms related to flight dynamics. |
GB/T 35853.4-2018: List of aerospace equivalent terms -- Part 4: Flight dynamics---This is a DRAFT version for illustration, not a final translation. Full copy of true-PDF in English version (including equations, symbols, images, flow-chart, tables, and figures etc.) will be manually/carefully translated upon your order.
List of aerospace equivalent terms.Part 4. Flight dynamics
National Standards of People's Republic of China
ICS 49.020
V 36
General Administration of Quality Supervision, Inspection and Quarantine of the People's Republic of China
China National Standardization Administration
release
Published on.2018-03-15
2018-10-01 Implementation
Aerospace equivalent glossary
Part 4. Flight dynamics
List of aerospace equivalent terms-
Part 4. Flight dynamics
(ISO 5843-4.1990, Aerospace-List of equivalent terms-
Part 4. Flight dynamics, MOD)
Foreword
GB/T 35853 "Aerospace Equivalent Glossary" is divided into nine parts.
-- Part 1. Aviation electrical equipment;
-- Part 2. Rivets for aerospace;
-- Part 3. Bolts and nuts for aerospace;
-- Part 4. Flight dynamics;
-- Part 5. Aircraft equipment environment and working conditions;
-- Part 6. Standard atmosphere;
-- Part 7. Aircraft reliability;
-- Part 8. Aircraft;
-- Part 9. Aircraft structure.
This part is the fourth part of GB/T 35853.
This part is drafted in accordance with the rules given in GB/T 1.1-2009.
This section uses the redrafting method to modify the use of ISO 5843-4.1990 "Aerospace equivalent glossary Part 4. Flying operations
Mechanics.
This section has made the following editorial changes.
- Change the standard name to "Aerospace equivalent glossary Part 4. Flight dynamics";
- deleted "Note 2" in the scope of ISO 5843-4.1990;
-- Removed the informative Appendix A of ISO 5843-4.1990 "ISO 5843-4 term number and ISO 1511 definition number
Control".
This part was proposed by China Aviation Industry Corporation.
This part is under the jurisdiction of the National Aircraft Standardization Technical Committee (SAC/TC 435).
This section drafted by. China Aviation Integrated Technology Research Institute, Beijing University of Aeronautics and Astronautics, China Flight Test Institute, Shaanxi Aircraft
Industry (Group) Co., Ltd., AVIC First Aircraft Design and Research Institute.
The main drafters of this section. Jia Xiao, Liu Qinzhi, Sun Wei, Qiu Zhiping, Shu Chenghui, Wang Haiqing, Wang Zhe, Wang Xianlun.
Aerospace equivalent glossary
Part 4. Flight dynamics
1 Scope
GB/T 35853 defines an equivalent glossary used in the field of aerospace facilities. This section gives terms related to flight dynamics.
Note. In addition to the three official languages of the International Organization for Standardization (ISO ) (English, French, Russian), the terms of ISO 5843 are given in German, etc.
Effective terminology. These terms are included in the ISO Technical Committee ISO /TC 20 application and are published under the responsibility of the German Member Body (DIN). Of course
However, terms given only in the official language can be used as ISO terms.
2 equivalent glossary
Serial number Chinese English French Russian German
Dimensionless tangential
Acceleration
Acceleration, normal-
Cited tangential
Accélération tangen-
Tielle réduite
Еезразмерное каса-
Тельное ускорение
Normierte Tangential-
Beschleu-nigung
Longitudinal speed
Rate of change
Row dimensionless
Derivative
Aero-normalized de-
Rival with respect
To the rate of change
Of the velocity compo-
Nent along the longitu-
Dinal axis
Dérivée sans dimension
Par rapport à la dérivée
De la composante de
La vitesse suivant l'axe
Long
Еезразмерная произ-
Водная по скорости
Изменения состав-
Ющяющей воздушной
Скорости вдоль про-
Оольной оси
Normiertes Deriva-
Tiv nach der zeitlichen
Ableitung der Gesch-
Windigkeitskompo-
Nente in Richtung der
Längsachse
Normal speed
Rate of change
Row dimensionless
Derivative
Aero-normalized de-
Rival with respect
To the rate of change
Of the velocity compo-
Nent along the normal
Align
Dérivée sans dimension
Par rapport à la dérivée
De la composante de
La vitesse suivant l'ахе
Normal
Еезразмерная произ-
Водная по скорости
Изменения состав-
Ющяющей воздушной
Скорости вдоль нор-
Мальной оси
Normiertes Deriva-
Tiv nach der zeitlichen
Ableitung der Gesch-
Windigkeitskompo-
Nente in Richtung der
Hochachse
Lateral speed
Rate of change
Row dimensionless
Derivative
Aero-normalized de-
Rival with respect
To the rate of change
Of the velocity compo-
Nent along the trans-
Verse axis
Dérivé sans dimension
Par rapport à la dérivée
De la composante de
La vitesse suivant l'ахе
Transversal
Еезразмерная произ-
Водная по скорости
Изменения состав-
Ющяющей воздушной
Скорости вдоль попе-
Речной оси
Normiertes Deriva-
Tiv nach der zeitlichen
Ableitung der Gesch-
Windigkeitskompo-
Nente in Richtung der
Querachse
Pitch rate
Aircraft without
Dimensional derivative
Aero-normalized deriv-
Aged with respect to
The rate of pitch
Dérivée sans dimension
Par rapport à la vitesse
De tangage
Еезразмерная произ-
Водная по скорости
Тангажа
Normiertes Deriva-
Tiv nach der Nickge-
Schwindigkeit
Roll rate
Aircraft without
Dimensional derivative
Aero-normalized deriv-
Aged with respect to
The rate of roll
Dérivée sans dimension
Par rapport à la vitesse
De roulis
Еезразмерная произ-
Водная no скорости
Крена
Normiertes Deriva-
Tiv nach der Rollge-
Schwindigkeit
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