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Real-Time Navigation Algorithm for the SHEFEX2 Hybrid Navigation System Experiment

Steffes, Stephen R. (2012) Real-Time Navigation Algorithm for the SHEFEX2 Hybrid Navigation System Experiment. AIAA Guidance, Navigation, and Control Conference, 13 - 16 August 2012, Minneapolis, Minnesota.

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Abstract

The Hybrid Navigation System was developed to achieve the required attitude accuracy and calculate a navigation solution for the SHEFEX2 mission, which launched on June 22, 2012 from And�ya Rocket Range in Norway by the German Aerospace Center (Deutsches- Zentrum f�ur Luft- und Raumfahrt, DLR). The real-time navigation algorithm fuses data from an IMU, GPS receiver, and star tracker using a delayed error state extended Kalman filter. The navigation algorithm uses a two part scheme to spread the work load and to ensure real-time requirements are met. Whole states are propagated at 400Hz as IMU data is available and the filter operations are done at 1Hz. A high-rate task propagates the whole states using a strapdown navigation routine, calculates the state transition matrix, maintains clock calibrations and executes part of the filter reset routine using the delayed error state estimates. A low-rate task propagates and updates the filter when measurement data is available. All measurements are synchronized to the GPS pulse per second signal so the sensor measurements have approximately the same reference time. Hardware-inthe- loop results show the navigation and computational performance of the algorithm in a real-time simulation.

Item URL in elib:https://elib.dlr.de/79772/
Document Type:Conference or Workshop Item (Paper)
Title:Real-Time Navigation Algorithm for the SHEFEX2 Hybrid Navigation System Experiment
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Steffes, Stephen R.stephen.steffes (at) dlr.deUNSPECIFIED
Date:2012
Refereed publication:No
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:Real-Time Navigation, SHEFEX2, Hybrid Navigation System, strapdown, GPS, IMU, Star tracker
Event Title:AIAA Guidance, Navigation, and Control Conference
Event Location:Minneapolis, Minnesota
Event Type:international Conference
Event Dates:13 - 16 August 2012
Organizer:AIAA
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Space
HGF - Program Themes:Space Transport
DLR - Research area:Raumfahrt
DLR - Program:R RP - Raumtransport
DLR - Research theme (Project):R - SHEFEX Programm (old)
Location: Bremen
Institutes and Institutions:Institute of Space Systems > Navigation and Control Systems
Deposited By: Steffes, Stephen
Deposited On:17 Jan 2013 10:58
Last Modified:12 Dec 2013 21:55

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