Paper information

Paper code

IAC-18,C4,8-B4.5A,4,x47325

Date

2018-10-05

Time

14:18

Order

4

Room

ZARM 5

Title

Hybrid Attitude and Orbit Control of a Pico-Satellite using Magnetic Torquers and an Electric Propulsion System

abstract

View PDF

Session

8-B4.5A. Joint Session between IAA and IAF for Small Satellite Propulsion Systems

symposium

C4. IAF SPACE PROPULSION SYMPOSIUM

congress

IAC-18

Type of presentation

oral

Main author

Mr. Philip Bangert, University Wuerzburg, Germany

Co-authors

Mr. Alexander Kramer, University of Würzburg, Germany;

Prof. Klaus Schilling, University Wuerzburg, Germany;