Flight results of GPS‐based attitude determination for the microsatellite Flying Laptop-Reference-Cited by-同舟云学术

Flight results of GPS‐based attitude determination for the microsatellite Flying Laptop

Published:2019-03-19 Issue:2 Volume:66 Page:277-287
ISSN:0028-1522
Container-title:Navigation
language:en
Short-container-title:NAVIGATION

Author:

Hauschild André¹^ORCID,Mohr Ulrich²,Markgraf Markus¹,Montenbruck Oliver¹^ORCID

Affiliation:

1. German Aerospace Center (DLR), German Space Operations Center (GSOC) Wessling Germany

2. University of StuttgartInstitute of Space Systems (IRS) Stuttgart Germany

Publisher

Institute of Navigation

Subject

Electrical and Electronic Engineering,Aerospace Engineering

Link

https://onlinelibrary.wiley.com/doi/pdf/10.1002/navi.299

Reference27 articles.

1. MontenbruckO MostertS NortierB.A miniature GPS receiver for precise orbit determination of the Sunsat 2004 micro‐satellite.Proceedings of the 2004 National Technical Meeting of The Institute of Navigation; January2004;San Diego CA:636‐642.

2. GrillmayerG FalkeA RöserH.Technology demonstration with the micro‐satellite Flying Laptop.Small Satellites for Earth Observation ‐ Selected Proceedings of the 5th International Symposium of the International Academy of Astronautics; April2005;Berlin Germany:419‐422.

3. WaidmannM SaileD GrillmayerG WolterV WaidmannC.Use of new developments on attitude control sensors for the microsatellite Flying Laptop.Proceedings of the 57th IAC/IAF/IAA (International Astronautical Congress); October2006;Valencia Spain.

4. SpinneyVW.Application of the Global Positioning System as an attitude reference for near‐Earth users.Proceedings of the Institute of Navigation National Aerospace Meeting; April1967;Warminster PA.

5. JosephKM DeemPS.Precision orientation: a new GPS application.International Telemetering Conference;San Diego CA:1983.

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