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Improved Hybrid Navigation for Space Transportation

Trigo, Guilherme Fragoso and Theil, Stephan (2017) Improved Hybrid Navigation for Space Transportation. 4th CEAS Eurognc Conference, 25-27 Apr 2017, Warsaw, Poland.

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This paper presents a tightly coupled hybrid navigation system for space transportation applications. The tightly integrated set-up, selected for its robustness and design flexibility, is here updated with GPS Pseudoranges and Time-Differenced GPS Carrier Phases (TDCP) to promote fast-dynamics estimation. The receiver clock errors affecting both GNSS observables are analysed and modelled. Tropospheric delay-rate is found to cause major disturbance to the TDCP during atmospheric ascent. A robust correction scheme for this effect is devised. Performance is evaluated using real GPS measurements.

Item URL in elib:https://elib.dlr.de/112254/
Document Type:Conference or Workshop Item (Lecture)
Title:Improved Hybrid Navigation for Space Transportation
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Trigo, Guilherme FragosoUNSPECIFIEDhttps://orcid.org/0000-0001-8173-9592UNSPECIFIED
Theil, StephanUNSPECIFIEDhttps://orcid.org/0000-0002-5346-8091UNSPECIFIED
Date:April 2017
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In ISI Web of Science:No
Keywords:Hybrid Navigation, GNSS, IMU, Kalman Filter, Launcher Navigation
Event Title:4th CEAS Eurognc Conference
Event Location:Warsaw, Poland
Event Type:international Conference
Event Dates:25-27 Apr 2017
Organizer:Council of European Aerospace Societies
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Space
HGF - Program Themes:Space Transportation
DLR - Research area:Raumfahrt
DLR - Program:R RP - Space Transportation
DLR - Research theme (Project):R - Project ReFEx - Reusability Flight Experiment
Location: Bremen
Institutes and Institutions:Institute of Space Systems > Navigation and Control Systems
Deposited By: Trigo, Guilherme Fragoso
Deposited On:09 May 2017 10:05
Last Modified:20 Aug 2021 10:18

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