FR2916868B1 - Procede et dispositif de determination de la marge de stabilite dynamique d'un avion. - Google Patents

Procede et dispositif de determination de la marge de stabilite dynamique d'un avion.

Info

Publication number
FR2916868B1
FR2916868B1 FR0755399A FR0755399A FR2916868B1 FR 2916868 B1 FR2916868 B1 FR 2916868B1 FR 0755399 A FR0755399 A FR 0755399A FR 0755399 A FR0755399 A FR 0755399A FR 2916868 B1 FR2916868 B1 FR 2916868B1
Authority
FR
France
Prior art keywords
aircraft
determining
dynamic stability
stability margin
margin
Prior art date
Legal status (The legal status 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 status listed.)
Expired - Fee Related
Application number
FR0755399A
Other languages
English (en)
Other versions
FR2916868A1 (fr
Inventor
Jerome Bazile
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Airbus Operations SAS
Original Assignee
Airbus Operations SAS
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 Airbus Operations SAS filed Critical Airbus Operations SAS
Priority to FR0755399A priority Critical patent/FR2916868B1/fr
Priority to US12/130,470 priority patent/US8265802B2/en
Publication of FR2916868A1 publication Critical patent/FR2916868A1/fr
Application granted granted Critical
Publication of FR2916868B1 publication Critical patent/FR2916868B1/fr
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • 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)
  • Engineering & Computer Science (AREA)
  • General Physics & Mathematics (AREA)
  • Pure & Applied Mathematics (AREA)
  • Mathematical Optimization (AREA)
  • Mathematical Physics (AREA)
  • Mathematical Analysis (AREA)
  • Algebra (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Automation & Control Theory (AREA)
  • Traffic Control Systems (AREA)
  • Navigation (AREA)
FR0755399A 2007-06-01 2007-06-01 Procede et dispositif de determination de la marge de stabilite dynamique d'un avion. Expired - Fee Related FR2916868B1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR0755399A FR2916868B1 (fr) 2007-06-01 2007-06-01 Procede et dispositif de determination de la marge de stabilite dynamique d'un avion.
US12/130,470 US8265802B2 (en) 2007-06-01 2008-05-30 Method and device for determining the dynamic stability margin of an aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0755399A FR2916868B1 (fr) 2007-06-01 2007-06-01 Procede et dispositif de determination de la marge de stabilite dynamique d'un avion.

Publications (2)

Publication Number Publication Date
FR2916868A1 FR2916868A1 (fr) 2008-12-05
FR2916868B1 true FR2916868B1 (fr) 2009-07-24

Family

ID=39103478

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0755399A Expired - Fee Related FR2916868B1 (fr) 2007-06-01 2007-06-01 Procede et dispositif de determination de la marge de stabilite dynamique d'un avion.

Country Status (2)

Country Link
US (1) US8265802B2 (fr)
FR (1) FR2916868B1 (fr)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP5550398B2 (ja) * 2010-03-18 2014-07-16 三菱重工業株式会社 舵面故障・損傷検出装置
FR3002334B1 (fr) * 2013-02-19 2016-07-15 Airbus Operations Sas Procede et dispositif d'estimation d'un moment de tangage non desire d'un avion, et applications au controle du tangage de l'avion.
US9669940B1 (en) * 2013-06-27 2017-06-06 Rockwell Collins, Inc. Latency-reducing image generating system, device, and method
CN106184811B (zh) * 2016-07-22 2018-05-22 北京临近空间飞行器***工程研究所 一种放宽偏航静稳定度的飞行器气动特性和控制设计方法
FR3057370B1 (fr) * 2016-10-11 2019-08-23 Airbus Operations Procede et systeme de commande de vol d'un aeronef.
CN109308074B (zh) * 2017-07-28 2021-10-08 深圳禾苗通信科技有限公司 一种无人机重心偏移的补偿方法及***
CN114296352B (zh) * 2021-12-31 2022-10-04 北京理工大学 一种高超声速飞行器的全局镇定控制方法及***

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2958483A (en) * 1953-08-03 1960-11-01 Northrop Corp Longitudinal stability augmenter
US4596368A (en) * 1983-10-21 1986-06-24 Schmittle Hugh J Ultralight aircraft with freely rotating wing
US4568043A (en) * 1983-10-21 1986-02-04 Schmittle Hugh J Ultra-light aircraft with freely rotating rigid wing
US4797829A (en) * 1986-12-11 1989-01-10 Grumman Aerospace Corporation Flight control optimization system for multi-control surface aircraft
JPH06255587A (ja) * 1993-03-09 1994-09-13 Honda Motor Co Ltd 航空機
US6341247B1 (en) * 1999-12-17 2002-01-22 Mcdonell Douglas Corporation Adaptive method to control and optimize aircraft performance
JP4171913B2 (ja) * 2004-04-13 2008-10-29 独立行政法人 宇宙航空研究開発機構 低ブーム特性と低抵抗特性を両立する可変前進翼超音速航空機
US7002349B2 (en) * 2004-06-24 2006-02-21 Telluric Exploration, Llc Remote sensing electric field exploration system

Also Published As

Publication number Publication date
FR2916868A1 (fr) 2008-12-05
US20090043432A1 (en) 2009-02-12
US8265802B2 (en) 2012-09-11

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