FR3040785B1 - Optimisation de la trajectoire de vol par programmation non lineaire - Google Patents
Optimisation de la trajectoire de vol par programmation non lineaire Download PDFInfo
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- FR3040785B1 FR3040785B1 FR1658136A FR1658136A FR3040785B1 FR 3040785 B1 FR3040785 B1 FR 3040785B1 FR 1658136 A FR1658136 A FR 1658136A FR 1658136 A FR1658136 A FR 1658136A FR 3040785 B1 FR3040785 B1 FR 3040785B1
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- 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.)
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- 238000005457 optimization Methods 0.000 title abstract 2
- 238000013178 mathematical model Methods 0.000 abstract 3
- 239000000446 fuel Substances 0.000 abstract 2
- 238000000034 method Methods 0.000 abstract 1
Classifications
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- 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
- G05D1/10—Simultaneous control of position or course in three dimensions
- G05D1/101—Simultaneous control of position or course in three dimensions specially adapted for aircraft
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- G—PHYSICS
- G08—SIGNALLING
- G08G—TRAFFIC CONTROL SYSTEMS
- G08G5/00—Traffic control systems for aircraft, e.g. air-traffic control [ATC]
- G08G5/0095—Aspects of air-traffic control not provided for in the other subgroups of this main group
-
- G—PHYSICS
- G08—SIGNALLING
- G08G—TRAFFIC CONTROL SYSTEMS
- G08G5/00—Traffic control systems for aircraft, e.g. air-traffic control [ATC]
- G08G5/003—Flight plan management
- G08G5/0034—Assembly of a flight plan
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
- G01C21/00—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00
- G01C21/20—Instruments for performing navigational calculations
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- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05B—CONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
- G05B13/00—Adaptive control systems, i.e. systems automatically adjusting themselves to have a performance which is optimum according to some preassigned criterion
- G05B13/02—Adaptive control systems, i.e. systems automatically adjusting themselves to have a performance which is optimum according to some preassigned criterion electric
- G05B13/04—Adaptive control systems, i.e. systems automatically adjusting themselves to have a performance which is optimum according to some preassigned criterion electric involving the use of models or simulators
-
- 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
- G05D1/0005—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots with arrangements to save energy
-
- G—PHYSICS
- G06—COMPUTING; CALCULATING OR COUNTING
- G06F—ELECTRIC DIGITAL DATA PROCESSING
- G06F17/00—Digital computing or data processing equipment or methods, specially adapted for specific functions
- G06F17/10—Complex mathematical operations
- G06F17/11—Complex mathematical operations for solving equations, e.g. nonlinear equations, general mathematical optimization problems
- G06F17/13—Differential equations
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- G—PHYSICS
- G06—COMPUTING; CALCULATING OR COUNTING
- G06F—ELECTRIC DIGITAL DATA PROCESSING
- G06F30/00—Computer-aided design [CAD]
- G06F30/10—Geometric CAD
- G06F30/15—Vehicle, aircraft or watercraft design
-
- G—PHYSICS
- G06—COMPUTING; CALCULATING OR COUNTING
- G06F—ELECTRIC DIGITAL DATA PROCESSING
- G06F30/00—Computer-aided design [CAD]
- G06F30/20—Design optimisation, verification or simulation
Landscapes
- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mathematical Physics (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Automation & Control Theory (AREA)
- Pure & Applied Mathematics (AREA)
- Mathematical Optimization (AREA)
- Computational Mathematics (AREA)
- Mathematical Analysis (AREA)
- Theoretical Computer Science (AREA)
- Data Mining & Analysis (AREA)
- Software Systems (AREA)
- Databases & Information Systems (AREA)
- General Engineering & Computer Science (AREA)
- Algebra (AREA)
- Operations Research (AREA)
- Evolutionary Computation (AREA)
- Computer Vision & Pattern Recognition (AREA)
- Artificial Intelligence (AREA)
- Medical Informatics (AREA)
- Health & Medical Sciences (AREA)
- Traffic Control Systems (AREA)
- Navigation (AREA)
- Feedback Control In General (AREA)
- Combined Controls Of Internal Combustion Engines (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
Abstract
Procédé (200), support et système pour recevoir une représentation, par un modèle mathématique, de caractéristiques de fonctionnement pour une combinaison d'un aéronef et d'un moteur ; effectuer sur la représentation par un modèle mathématique une réduction d'ordre du modèle par projection ; éliminer, d'après le modèle projeté, des composantes de dynamique rapide de la représentation par modèle mathématique ; déterminer un modèle à ordre réduit, sous la forme d'une équation algébrique différentielle dans laquelle des équations algébriques remplacent la dynamique rapide ; établir un angle de trajectoire de vol et un angle de manette des gaz comme commande pour limiter fortement la consommation de carburant pour la combinaison d'un aéronef et d'un moteur modélisés ; discrétiser des équations de mouvement pour la combinaison d'un aéronef et d'un moteur modélisés et formuler des équations d'optimisation sous la forme d'un problème de programmation non linéaire ; et déterminer une commande optimale en boucle ouverte qui limite fortement la consommation de carburant pour la combinaison d'un aéronef et d'un moteur modélisés afin de monter jusqu'à atteindre une altitude et une vitesse propre prescrites.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US14/844,892 US9564056B1 (en) | 2015-09-03 | 2015-09-03 | Flight path optimization using nonlinear programming |
US14/844.892 | 2015-09-03 |
Publications (2)
Publication Number | Publication Date |
---|---|
FR3040785A1 FR3040785A1 (fr) | 2017-03-10 |
FR3040785B1 true FR3040785B1 (fr) | 2019-12-20 |
Family
ID=57119903
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1658136A Active FR3040785B1 (fr) | 2015-09-03 | 2016-09-01 | Optimisation de la trajectoire de vol par programmation non lineaire |
Country Status (7)
Country | Link |
---|---|
US (1) | US9564056B1 (fr) |
JP (1) | JP6212610B2 (fr) |
CN (1) | CN106502263B (fr) |
BR (1) | BR102016020326A2 (fr) |
CA (1) | CA2940044C (fr) |
FR (1) | FR3040785B1 (fr) |
GB (1) | GB2543902B (fr) |
Families Citing this family (23)
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US10604268B2 (en) * | 2017-02-22 | 2020-03-31 | Pratt & Whitney Canada Corp. | Autothrottle control for turboprop engines |
CN106686258A (zh) * | 2017-03-14 | 2017-05-17 | 深圳市乐升科技有限公司 | 一种可拆卸无人机的控制方法及*** |
US20180286253A1 (en) * | 2017-03-31 | 2018-10-04 | General Electric Company | Optimized aircraft control via model-based iterative optimization |
FR3067491B1 (fr) * | 2017-06-08 | 2019-07-05 | Airbus (S.A.S.) | Dispositif, systeme et procede d'assistance a un pilote d'un aeronef |
US20190005826A1 (en) * | 2017-06-28 | 2019-01-03 | Ge Aviation Systems, Llc | Engine load model systems and methods |
US10953995B2 (en) | 2017-06-30 | 2021-03-23 | General Electric Company | Propulsion system for an aircraft |
US10569759B2 (en) | 2017-06-30 | 2020-02-25 | General Electric Company | Propulsion system for an aircraft |
US10738706B2 (en) | 2017-06-30 | 2020-08-11 | General Electric Company | Propulsion system for an aircraft |
US10696416B2 (en) | 2017-06-30 | 2020-06-30 | General Electric Company | Propulsion system for an aircraft |
US10388170B2 (en) | 2017-08-14 | 2019-08-20 | Honeywell International Inc. | Speed-constrained flight management methods and systems |
US10671092B2 (en) * | 2017-10-20 | 2020-06-02 | The Boeing Company | Airplane climb thrust optimization |
CN108717265B (zh) * | 2018-05-30 | 2021-05-18 | 重庆邮电大学 | 一种基于控制变量参数化的无人飞行器巡航跟踪控制***及控制方法 |
US11142337B2 (en) | 2018-07-17 | 2021-10-12 | Ge Aviation Systems Llc | Method and system for determining a descent profile |
US10935984B2 (en) | 2018-07-17 | 2021-03-02 | Ge Aviation Systems Llc | Method and system for determining a climb profile |
CN109159909B (zh) * | 2018-07-25 | 2022-02-22 | 中国航空工业集团公司沈阳飞机设计研究所 | 临近空间高速飞机爬升轨迹的设计方法 |
CN111796516B (zh) * | 2019-04-03 | 2024-07-19 | 北京京东乾石科技有限公司 | 用于规划轨迹的方法和装置 |
CN110466804B (zh) * | 2019-08-30 | 2021-04-09 | 北京理工大学 | 火箭动力下降着陆过程快速轨迹优化方法 |
CN111209629B (zh) * | 2019-11-16 | 2021-08-31 | 中国科学院力学研究所 | 宽域飞行器总体参数优化方法、***及计算机存储介质 |
CN111338364B (zh) * | 2019-11-21 | 2021-09-21 | 浙江大学 | 快速响应的高超声速飞行器轨迹优化高精度控制器 |
CN112348228B (zh) * | 2020-09-28 | 2022-05-17 | 北京航空航天大学 | 一种基于高度-航程剖面的飞行器速度预测方法 |
US20220101735A1 (en) * | 2020-09-30 | 2022-03-31 | At&T Intellectual Property I, L.P. | System and method for navigation of unmanned aerial vehicles using mobile networks |
CN112231943B (zh) * | 2020-12-17 | 2021-02-26 | 中国人民解放军国防科技大学 | 含“一石多鸟”飞越片段的多星飞越序列搜索方法与*** |
CN113721663B (zh) * | 2021-10-29 | 2023-03-21 | 北京航空航天大学 | 一种柔性飞行器的起降轨迹规划方法 |
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US5908176A (en) | 1997-01-14 | 1999-06-01 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | In-flight adaptive performance optimization (APO) control using redundant control effectors of an aircraft |
WO1998047765A1 (fr) * | 1997-04-24 | 1998-10-29 | Galaxy Development, Llc. | Changements d'inclinaison de satellite a l'aide de limites de stabilite faibles |
US6244536B1 (en) * | 1997-11-26 | 2001-06-12 | The United States Of America As Represented By The Secretary Of The Air Force | Air to air homing missile guidance |
US6266610B1 (en) * | 1998-12-31 | 2001-07-24 | Honeywell International Inc. | Multi-dimensional route optimizer |
US6134500A (en) | 1999-06-03 | 2000-10-17 | United Air Lines, Inc. | System and method for generating optimal flight plans for airline operations control |
FR2857480B1 (fr) * | 2003-07-07 | 2005-09-30 | Airbus France | Procede et dispositif de generation d'un plan de vol pour un vol tactique d'un aeronef |
US20090177339A1 (en) * | 2005-03-03 | 2009-07-09 | Chen Robert H | Optimization and Mechanization of Periodic Flight |
US8128034B2 (en) * | 2005-08-15 | 2012-03-06 | Abe Karem | Rotorcraft with opposing roll mast moments, and related methods |
US8157205B2 (en) * | 2006-03-04 | 2012-04-17 | Mcwhirk Bruce Kimberly | Multibody aircrane |
JP4473899B2 (ja) * | 2007-08-10 | 2010-06-02 | 株式会社東芝 | 航法支援装置、この航法支援装置を搭載する航空機、および航法支援方法 |
FR2946780B1 (fr) * | 2009-06-12 | 2011-07-15 | Thales Sa | Procede et dispositif d'affichage des limites de marges de vol pour un aeronef |
CN101625571B (zh) * | 2009-07-25 | 2010-12-29 | 大连理工大学 | 一种模拟自旋式飞行器六自由度运动的方法 |
CN101833335B (zh) * | 2010-05-10 | 2013-10-30 | 珠海云洲智能科技有限公司 | 小型水面机器人装置及自适应水流优化导航方法 |
US20120078450A1 (en) * | 2010-09-27 | 2012-03-29 | Honeywell International Inc. | Display information to support climb optimization during cruise |
CN102114914B (zh) * | 2011-01-21 | 2014-03-19 | 文杰 | 分布式动力多旋翼垂直起降飞行器及其控制方法 |
US8594917B2 (en) | 2011-01-25 | 2013-11-26 | Nextgen Aerosciences, Llc | Method and apparatus for dynamic aircraft trajectory management |
US20120265374A1 (en) * | 2011-04-15 | 2012-10-18 | Thomas Edward Yochum | Aircraft vertical trajectory optimization method |
US8909395B2 (en) * | 2011-04-29 | 2014-12-09 | Airbus Engineering Centre India | System and method for aircraft performance predictions for climb flight phase |
US8857412B2 (en) * | 2011-07-06 | 2014-10-14 | General Electric Company | Methods and systems for common rail fuel system dynamic health assessment |
US8682512B2 (en) * | 2011-12-16 | 2014-03-25 | General Electric Company | Fuel optimizing system for a mobile asset, and a related method thereof |
DE102012001268A1 (de) | 2012-01-23 | 2013-07-25 | Airbus Operations Gmbh | Verfahren zur Planung eines Landeanflugs eines Flugzeugs, Computerprogrammprodukt, Medium mit einem darauf gespeicherten Landeanflugplan sowie Vorrichtung zur Planung eines Landeanflugs |
US8655589B2 (en) | 2012-01-25 | 2014-02-18 | Mitsubishi Electric Research Laboratories, Inc. | System and method for controlling motion of spacecrafts |
US8645009B2 (en) * | 2012-02-23 | 2014-02-04 | Ge Aviation Systems Llc | Method for flying an aircraft along a flight path |
US8825237B2 (en) | 2012-04-26 | 2014-09-02 | Bell Helicopter Textron Inc. | System and method for economic usage of an aircraft |
US20140018980A1 (en) * | 2012-07-12 | 2014-01-16 | General Electric Company | Systems and methods for flight management |
CN103970143B (zh) * | 2013-08-27 | 2017-03-29 | 清华大学 | 一种无人飞行器自主巡点飞行的智能优化方法 |
FR3012630B1 (fr) * | 2013-10-25 | 2016-01-01 | Thales Sa | Procede d'aide a la navigation pour un aeronef en descente et en approche a poussee reduite |
CN104309822B (zh) | 2014-11-04 | 2016-04-27 | 哈尔滨工业大学 | 一种基于参数优化的航天器单脉冲水滴形绕飞轨迹悬停控制方法 |
JP6517104B2 (ja) * | 2015-07-17 | 2019-05-22 | 三菱重工業株式会社 | 航空機管理装置、航空機、及び航空機の軌道算出方法 |
-
2015
- 2015-09-03 US US14/844,892 patent/US9564056B1/en active Active
-
2016
- 2016-08-23 JP JP2016162309A patent/JP6212610B2/ja not_active Expired - Fee Related
- 2016-08-25 CA CA2940044A patent/CA2940044C/fr active Active
- 2016-08-31 CN CN201610771123.4A patent/CN106502263B/zh active Active
- 2016-08-31 GB GB1614691.2A patent/GB2543902B/en active Active
- 2016-09-01 FR FR1658136A patent/FR3040785B1/fr active Active
- 2016-09-02 BR BR102016020326A patent/BR102016020326A2/pt not_active Application Discontinuation
Also Published As
Publication number | Publication date |
---|---|
CN106502263A (zh) | 2017-03-15 |
CA2940044A1 (fr) | 2017-03-03 |
GB2543902B (en) | 2018-02-28 |
US9564056B1 (en) | 2017-02-07 |
JP6212610B2 (ja) | 2017-10-11 |
CA2940044C (fr) | 2018-10-09 |
CN106502263B (zh) | 2020-01-10 |
BR102016020326A2 (pt) | 2017-03-07 |
FR3040785A1 (fr) | 2017-03-10 |
JP2017074940A (ja) | 2017-04-20 |
GB2543902A (en) | 2017-05-03 |
GB201614691D0 (en) | 2016-10-12 |
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