Zobrazeno 1 - 7
of 7
pro vyhledávání: '"Michael Frangenberg"'
Autor:
Johannes Schneider, Michael Frangenberg, Stefan Notter, Werner Scholz, Walter Fichter, Andreas Strohmayer
Publikováno v:
CEAS Aeronautical Journal. 13:861-876
In this practical approach to distributed propulsion, the solar-powered manned motorglider icaré 2 has been used as a testbed for wingtip propulsion. The large wingspan and slow cruising speed of icaré 2 are highly suitable to assess the influence
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::43f5707868c1a058668a333787c5c81e
https://doi.org/10.1007/s13272-022-00603-4
https://doi.org/10.1007/s13272-022-00603-4
Autor:
Jan Denzel, Walter Fichter, Andreas Strohmayer, Ole Pfeifle, Johannes Schneider, Werner Scholz, Michael Frangenberg, Stefan Notter, Dominique Paul Bergmann
Publikováno v:
AIAA AVIATION 2021 FORUM.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f257d6d36fc3fafd00f4ac687a7d16eb
https://doi.org/10.2514/6.2021-3192
https://doi.org/10.2514/6.2021-3192
Publikováno v:
Journal of Guidance, Control, and Dynamics. 39:970-978
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::88787f58aa66156f22404bead2e78268
https://doi.org/10.2514/1.g001134
https://doi.org/10.2514/1.g001134
Publikováno v:
Journal of Guidance, Control, and Dynamics. 38:506-518
In this paper, a particle filter is proposed to estimate attitude and velocity onboard a small unmanned aerial system using GPS, gyro, and accelerometer measurements. For the proposed filter setup, attitude observability heavily depends on the vehicl
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::3b942d6613f646a40633c09b3530f392
https://doi.org/10.2514/1.g000238
https://doi.org/10.2514/1.g000238
Publikováno v:
AIAA Guidance, Navigation, and Control Conference.
Motor failures pose a significant problem for the autonomous operation of multicopters. On the one hand the fault has to be detected and on the other hand the remaining asymmetric actuator envelope has to be fully exploited to maintain control of the
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::07e01c51b39712c966ff44293ddf117c
https://doi.org/10.2514/6.2015-1766
https://doi.org/10.2514/6.2015-1766
Publikováno v:
AIAA Guidance, Navigation, and Control (GNC) Conference.
In this paper, a particle filter (PF) is proposed to estimate attitude and velocity on board a mini aerial vehicle (MAV) using only GPS measurements in the re-weighting step. The attitude observability of the system heavily depends on the vehicle tra
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::866f7859ec58b946c455c37b8a254c05
https://doi.org/10.2514/6.2013-5247
https://doi.org/10.2514/6.2013-5247