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Source: https://mediatum.ub.tum.de/603817?show_id=1335434 Parent: https://www.fsd.ed.tum.de/staff-members/johann-dambeck/

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mediaTUM Gesamtbestand Elektronische Prüfungsarbeiten Fachgebiet Meßtechnik, Steuerungs- und Regelungstechnik, Automation


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Original title: : Platform-autonomous Fault-tolerant Attitude/Heading Reference and Navigation Systems

Translated title: : Plattformautonome fehlertolerante Kurs-Lage-Referenz- und Navigationssysteme

Author: : Baklanov, Fedor

Year: : 2017

Document type: : Dissertation

Faculty/School: : Fakultät für Maschinenwesen

Advisor: : Holzapfel, Florian (Prof. Dr.)

Referee: : Holzapfel, Florian (Prof. Dr.); Kleusberg, Alfred (Prof. Dr.)

Language: : en

Subject group: : MSR Meßtechnik, Steuerungs- und Regelungstechnik, Automation; VER Technik der Verkehrsmittel

Keywords: : AHRS, IMU, air data, magnetometer, integrated navigation, observability

TUM classification: : VER 500d

Abstract: : This thesis investigates possibility to improve reliability and performance of low-cost aeronautical integrated navigation systems by making use of robust autonomous measurements, namely of inertial measurement unit, air data system, and 3-axis magnetometer. The central applied result of the research consists in proposing low size, weight, power, and cost design of a robust platform-autonomous fault-tolerant navigation system with the best in-IMU-class performance, which, in the events of failures, can gracefully degrade to attitude and heading reference system. «

This thesis investigates possibility to improve reliability and performance of low-cost aeronautical integrated navigation systems by making use of robust autonomous measurements, namely of inertial measurement unit, air data system, and 3-axis magnetometer. The central applied result of the research consists in proposing low size, weight, power, and cost design of a robust platform-autonomous fault-tolerant navigation system with the best in-IMU-class performance, which, in the events of failur...    
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Translated abstract: : Diese Arbeit untersucht die Möglichkeit die Zuverlässigkeit und Leistung kostengünstiger, integrierter Navigationssysteme für die Luftfahrt zu verbessern. Hierzu werden robuste, autonome Messungen wie etwa aus der Inertialen Messeinheit, Luftdaten sowie 3-Achsen Magnetometer verwendet. Als zentrales, anwendbares Ergebnis dieser Forschung der Entwurf eines kleinen, leichten und kostengünstigen plattform-autonomen fehlertoleranten Navigationssystems vorgeschlagen.

WWW: : https://mediatum.ub.tum.de/?id=1335434

Date of submission: : 10.11.2016

Oral examination: : 24.05.2017

File size: : 16349134 bytes

Pages: : 219

Urn (citeable URL): : https://nbn-resolving.org/urn:nbn:de:bvb:91-diss-20170524-1335434-1-1

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