FR3040785B1 - Optimisation de la trajectoire de vol par programmation non lineaire - Google Patents

Optimisation de la trajectoire de vol par programmation non lineaire Download PDF

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Publication number
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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engine
combination
model
representation
aircraft
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FR3040785A1 (fr
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Reza Ghaemi
Eric Richard Westervelt
Mark Darnell
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General Electric Co
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General Electric Co
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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
    • G—PHYSICS
    • G08—SIGNALLING
    • G08G—TRAFFIC CONTROL SYSTEMS
    • G08G5/00—Traffic control systems for aircraft
    • 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
    • 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 OR CALCULATING; 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
    • G—PHYSICS
    • G08—SIGNALLING
    • G08G—TRAFFIC CONTROL SYSTEMS
    • G08G5/00—Traffic control systems for aircraft
    • G08G5/30—Flight plan management
    • G08G5/32—Flight plan management for flight plan preparation
    • G—PHYSICS
    • G06—COMPUTING OR CALCULATING; 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 OR CALCULATING; COUNTING
    • G06F—ELECTRIC DIGITAL DATA PROCESSING
    • G06F30/00—Computer-aided design [CAD]
    • G06F30/20—Design optimisation, verification or simulation

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  • 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)
  • Computational Mathematics (AREA)
  • Mathematical Analysis (AREA)
  • Mathematical Optimization (AREA)
  • Pure & Applied Mathematics (AREA)
  • Theoretical Computer Science (AREA)
  • Data Mining & Analysis (AREA)
  • Software Systems (AREA)
  • Algebra (AREA)
  • General Engineering & Computer Science (AREA)
  • Databases & Information Systems (AREA)
  • Operations Research (AREA)
  • Medical Informatics (AREA)
  • Evolutionary Computation (AREA)
  • Health & Medical Sciences (AREA)
  • Computer Vision & Pattern Recognition (AREA)
  • Artificial Intelligence (AREA)
  • Traffic Control Systems (AREA)
  • Navigation (AREA)
  • Feedback Control In General (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Combined Controls Of Internal Combustion Engines (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.
FR1658136A 2015-09-03 2016-09-01 Optimisation de la trajectoire de vol par programmation non lineaire Active FR3040785B1 (fr)

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

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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 (31)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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系统
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
US10696416B2 (en) 2017-06-30 2020-06-30 General Electric Company Propulsion system for an aircraft
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
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系统及控制方法
US10935984B2 (en) 2018-07-17 2021-03-02 Ge Aviation Systems Llc Method and system for determining a climb profile
US11142337B2 (en) 2018-07-17 2021-10-12 Ge Aviation Systems Llc Method and system for determining a descent 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
GB201909464D0 (en) * 2019-07-01 2019-08-14 Rolls Royce Plc Aircraft control method
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、系统及计算机存储介质
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系统
AU2022380638B2 (en) * 2021-08-19 2024-11-28 Merlin Labs, Inc. Advanced flight processing system and/or method
GB2610200B (en) 2021-08-25 2024-11-20 Rolls Royce Plc Computer-implemented methods of enabling optimisation of trajectory for a vehicle
GB2610199B (en) * 2021-08-25 2024-01-17 Rolls Royce Plc Computer-implemented methods for enabling optimisation of derate for a propulsion system of a vehicle
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
US12480449B2 (en) 2022-08-22 2025-11-25 General Electric Company Propulsion system including an electric machine for starting a gas turbine engine
CN118938680B (zh) * 2024-08-15 2025-05-23 西北工业大学 一种基于伪谱法的飞行器任务剖面规划仿真分析方法
CN119960288B (zh) * 2025-01-20 2025-10-17 中国人民解放军海军工程大学 一种航行器水面发射控制方法
CN120840888B (zh) * 2025-09-25 2025-12-09 中国民用航空飞行学院 一种飞行管理系统的等表速和马赫数爬升性能确定方法

Family Cites Families (29)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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
AU738202B2 (en) * 1997-04-24 2001-09-13 Galaxy Development, Llc. Satellite inclination changes using weak stability boundaries
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
WO2012103228A1 (fr) 2011-01-25 2012-08-02 Nextgen Aerosciences, Llc Procédé et appareil de gestion dynamique de trajectoires d'aéronefs
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

Also Published As

Publication number Publication date
GB201614691D0 (en) 2016-10-12
BR102016020326A2 (pt) 2017-03-07
FR3040785A1 (fr) 2017-03-10
CN106502263B (zh) 2020-01-10
JP2017074940A (ja) 2017-04-20
GB2543902B (en) 2018-02-28
GB2543902A (en) 2017-05-03
JP6212610B2 (ja) 2017-10-11
CA2940044C (fr) 2018-10-09
US9564056B1 (en) 2017-02-07
CN106502263A (zh) 2017-03-15
CA2940044A1 (fr) 2017-03-03

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