P.A. Krauss, M. Hartrampf, A. Barrios-Montalvo, E. Gottzein

The presentation demonstrates the feasibility of on-board autonomous orbit determination using GNSS for spacecraft in transfer to geostationary orbit focusing on chemical and electrical propulsion. GNSS navigation performance is analyzed by HW-in-the-loop tests using different transfer scenarios. Transfer scenarios are derived from realistic spacecraft orbit, attitude and acceleration profiles in particular of the Electra spacecraft, which were kindly provided by OHB Sweden. The HW-in-the-loop tests are done with the Airbus Defence and Space LION Navigator GNSS receiver engineering model (EM) featuring enhanced software and the Spirent Simulator GSS 9000.

Deutscher Luft- und Raumfahrtkongress 2017, München

Deutsche Gesellschaft für Luft- und Raumfahrt - Lilienthal-Oberth e.V., Bonn, 2017

Conference Paper

englisch

21,0 x 29,7 cm, 12 Seiten

urn:nbn:de:101:1-201712013535

Onboard Autonomy, Space Service Volume

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01.12.2017