Accurate State-Space Inflow Modeling for Flight Dynamics and Control of a Coaxial-Pusher Rotorcraft
American Helicopter Society (International annual forum)
01.01.2018
18 pages
Aufsatz (Konferenz)
Englisch
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
INFLOW SYSTEM IDENTIFICATION FOR COAXIAL-PUSHER ROTORCRAFT IN CRUISING FLIGHT
| British Library Conference Proceedings | 2019
Multidisciplinary Trim Analysis of a Coaxial-Pusher Rotorcraft Configuration
| British Library Conference Proceedings | 2018
Flight Dynamics Modeling of Coaxial Rotorcraft UAVs
| Springer Verlag | 2014