ES2028905T3 - Sistema de referencia redundante, integrado para la regulacion del vuelo y para la generacion de informacion del rumbo y de la posicion. - Google Patents

Sistema de referencia redundante, integrado para la regulacion del vuelo y para la generacion de informacion del rumbo y de la posicion.

Info

Publication number
ES2028905T3
ES2028905T3 ES198787730109T ES87730109T ES2028905T3 ES 2028905 T3 ES2028905 T3 ES 2028905T3 ES 198787730109 T ES198787730109 T ES 198787730109T ES 87730109 T ES87730109 T ES 87730109T ES 2028905 T3 ES2028905 T3 ES 2028905T3
Authority
ES
Spain
Prior art keywords
information
elements
flight
integrated
acceleration
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
ES198787730109T
Other languages
English (en)
Inventor
Uwe Krogmann
Jurgen Bessel
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.)
Bodenseewerk Geratetechnik GmbH
Original Assignee
Bodenseewerk Geratetechnik 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 Bodenseewerk Geratetechnik GmbH filed Critical Bodenseewerk Geratetechnik GmbH
Application granted granted Critical
Publication of ES2028905T3 publication Critical patent/ES2028905T3/es
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • 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
    • G01C21/10—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by using measurements of speed or acceleration
    • G01C21/12—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by using measurements of speed or acceleration executed aboard the object being navigated; Dead reckoning
    • G01C21/16—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by using measurements of speed or acceleration executed aboard the object being navigated; Dead reckoning by integrating acceleration or speed, i.e. inertial navigation
    • G01C21/183—Compensation of inertial measurements, e.g. for temperature effects

Landscapes

  • Engineering & Computer Science (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Automation & Control Theory (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Navigation (AREA)
  • Gyroscopes (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)

Abstract

UNA VARIEDAD DE GIROSCOPOS INVERSORES DE DOS EJES ESTAN DISPUESTOS ESTACIONARIAMENTE EL AVION, YA QUE SUMINISTRAN REDONDAMENTE INFORMACIONES SOBRE VELOCIDADES ANGULARES. UNA VARIEDAD DE INDICADORES DE ACELERACION SUMINISTRAN REDONDANTEMENTE INFORMACIONES DE ACELERACION. PRIMEROS ELEMENTOS DE ELABORACION DE SEÑALES CONTIENEN ELEMENTOS PARA EL RECONOCIMIENTO DE DEFECTOS Y DESCONEXION AUTOMATICA Y ELEMENTOS PARA ELIMINAR INFORMACIONES DE VELOCIDADES ANGULARES Y DE ACELERACION DEFECTUOSAS. LAS INFORMACIONES DE VELOCIDADES ANGULARES Y ACELERACIONES LIBRES DE ERRORES SUMINISTRAN SEÑALES ESTABLES PARA REGULAR EL AVION. SEGUNDOS ELEMENTOS DE ELABORACION DE SEÑALES CONTIENEN INFORMACIONES DE VELOCIDADES ANGULARES Y DE ACELERACIONES LIBRES DE DEFECTOS E INTEGRADAS Y SUMINISTRAN SEÑALES DE REFERENCIA SOBRE EL VUELO Y LA SITUACION DEL AVION.
ES198787730109T 1986-10-07 1987-09-21 Sistema de referencia redundante, integrado para la regulacion del vuelo y para la generacion de informacion del rumbo y de la posicion. Expired - Lifetime ES2028905T3 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19863634023 DE3634023A1 (de) 1986-10-07 1986-10-07 Integriertes, redundantes referenzsystem fuer die flugregelung und zur erzeugung von kurs- und lageinformationen

Publications (1)

Publication Number Publication Date
ES2028905T3 true ES2028905T3 (es) 1992-07-16

Family

ID=6311169

Family Applications (1)

Application Number Title Priority Date Filing Date
ES198787730109T Expired - Lifetime ES2028905T3 (es) 1986-10-07 1987-09-21 Sistema de referencia redundante, integrado para la regulacion del vuelo y para la generacion de informacion del rumbo y de la posicion.

Country Status (4)

Country Link
US (1) US4914598A (es)
EP (1) EP0263777B1 (es)
DE (2) DE3634023A1 (es)
ES (1) ES2028905T3 (es)

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RU2747672C1 (ru) * 2020-03-24 2021-05-12 федеральное государственное казенное военное образовательное учреждение высшего образования "Краснодарское высшее военное орденов Жукова и Октябрьской Революции Краснознаменное училище имени генерала армии С.М. Штеменко" Министерства обороны Российской Федерации Устройство преобразования сигналов датчиков углов беспилотного летательного аппарата в кватернионы
CN111498142B (zh) * 2020-05-06 2021-12-14 南京航空航天大学 一种飞机航电成品安装校准方法
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CN113532482B (zh) * 2021-08-10 2022-11-11 湖北航天技术研究院总体设计所 一种冗余惯性测量***故障检测装置及检测方法
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Also Published As

Publication number Publication date
US4914598A (en) 1990-04-03
EP0263777B1 (de) 1991-12-11
DE3775163D1 (de) 1992-01-23
EP0263777A3 (en) 1990-02-14
DE3634023A1 (de) 1988-04-21
EP0263777A2 (de) 1988-04-13

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