ES2133641T3 - Procedimiento para la generacion de una trayectoria de vuelo. - Google Patents

Procedimiento para la generacion de una trayectoria de vuelo.

Info

Publication number
ES2133641T3
ES2133641T3 ES95115835T ES95115835T ES2133641T3 ES 2133641 T3 ES2133641 T3 ES 2133641T3 ES 95115835 T ES95115835 T ES 95115835T ES 95115835 T ES95115835 T ES 95115835T ES 2133641 T3 ES2133641 T3 ES 2133641T3
Authority
ES
Spain
Prior art keywords
determined
land
route
horizontal
air route
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 - Lifetime
Application number
ES95115835T
Other languages
English (en)
Inventor
Klaus-Dieter Dr Kricke
Dirk Schafer
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 Defence and Space GmbH
Airbus Operations GmbH
Original Assignee
DaimlerChrysler Aerospace AG
Airbus Operations GmbH
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 DaimlerChrysler Aerospace AG, Airbus Operations GmbH filed Critical DaimlerChrysler Aerospace AG
Application granted granted Critical
Publication of ES2133641T3 publication Critical patent/ES2133641T3/es
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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
    • G05D1/04—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
    • G05D1/0646—Rate of change of altitude or depth specially adapted for aircraft to follow the profile of undulating ground
    • 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
    • G01C21/005—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 with correlation of navigation data from several sources, e.g. map or contour matching

Landscapes

  • Engineering & Computer Science (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Automation & Control Theory (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Navigation (AREA)
  • Traffic Control Systems (AREA)

Abstract

EL PROCEDIMIENTO SIRVE PARA LA GENERACION INTERACTIVA DE UNA RUTA AEREA PROXIMA AL SUELO, EN DEPENDENCIA DE LA PERFILACION DEL TERRENO MEDIANTE VALORACION DE LOS DATOS DE TERRENO ALMACENADOS DIGITALES. PARA UNA PARTE DE TERRENO A SER SOBREVOLADA SE DETERMINA UN PUNTO DE COMIENZO DEL VUELO Y UN PUNTO DE TERMINACION. A CONTINUACION SE DETERMINA UNA VIA DE UNION HORIZONTAL ENTRE EL PUNTO DE COMIENZO Y EL PUNTO DE TERMINACION. LA VIA DE UNION HORIZONTAL SE DETERMINA MEDIANTE VALORACION DE LINEAS DE ALTURA DE LOS DATOS DE TERRENO DIGITALES DE TAL MODO, QUE RESULTA UNA RUTA AEREA HORIZONTAL SOBRE UN PLANO HORIZONTAL REDUCIDO. LA RUTA AEREA HORIZONTAL SE SUBDIVIDE EN SEGMENTOS DE RUTA ESENCIALMENTE LINEALES CON TRANSCONEXION CURVADA PREVIAMENTE DADA. PARA CADA ELEMENTO DE RUTA AEREA SE DETERMINA UNA MODIFICACION DE ALTURA DE VUELO VERTICAL DE FORMA AUTOMATICA MEDIANTE VALORACION DE LOS DATOS DEL TERRENO DIGITALES.
ES95115835T 1994-10-12 1995-10-07 Procedimiento para la generacion de una trayectoria de vuelo. Expired - Lifetime ES2133641T3 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE4436356A DE4436356B4 (de) 1994-10-12 1994-10-12 Verfahren zur Flugweggenerierung

Publications (1)

Publication Number Publication Date
ES2133641T3 true ES2133641T3 (es) 1999-09-16

Family

ID=6530518

Family Applications (1)

Application Number Title Priority Date Filing Date
ES95115835T Expired - Lifetime ES2133641T3 (es) 1994-10-12 1995-10-07 Procedimiento para la generacion de una trayectoria de vuelo.

Country Status (3)

Country Link
EP (1) EP0707194B1 (es)
DE (2) DE4436356B4 (es)
ES (1) ES2133641T3 (es)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE10308913A1 (de) * 2003-02-28 2004-09-30 Ais Advanced Infodata Systems Gmbh Flugsicherungssystem und hierzu verwendete Repräsentation der Erdoberfläche
FR2870515B1 (fr) * 2004-05-18 2007-08-03 Airbus France Sas Procede et dispositif de revision d'un plan de vol d'un aeronef
FR2947370B1 (fr) * 2009-06-26 2011-11-25 Eurocopter France Procede d'aide au pilotage a basse altitude
US8645009B2 (en) * 2012-02-23 2014-02-04 Ge Aviation Systems Llc Method for flying an aircraft along a flight path
CN113377128B (zh) * 2021-06-10 2022-12-09 北京空天技术研究所 一种飞行器可达区域估算方法
CN113447000B (zh) * 2021-06-26 2022-06-21 珠海经济特区建设监理有限公司 超高层建筑工程测量的监理控制方法、系统、设备及介质
CN114018263A (zh) * 2021-10-27 2022-02-08 南京壮大智能科技研究院有限公司 飞行汽车行驶路线规划方法
CN117320106B (zh) * 2023-11-30 2024-03-12 湖南林科达信息科技有限公司 一种基于北斗的林业无人机智能通信系统及终端

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2907549C2 (de) * 1979-02-26 1985-11-21 The Boeing Co., Seattle, Wash. Verfahren und Vorrichtung zum Steuern der Fahrhöhe eines Fahrzeuges oberhalb einer minimal zulässigen Höhe
DE3604401A1 (de) * 1986-02-12 1987-08-20 Messerschmitt Boelkow Blohm Tiefflugverfahren zur automatischen kursbestimmung
FR2658636B1 (fr) * 1990-02-22 1994-08-26 Sextant Avionique Procede de pilotage d'un aeronef en vol a tres basse altitude.

Also Published As

Publication number Publication date
EP0707194B1 (de) 1999-05-19
DE4436356B4 (de) 2007-10-31
DE4436356A1 (de) 1996-04-25
DE59505961D1 (de) 1999-06-24
EP0707194A1 (de) 1996-04-17

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