On the scalability of experimentally determined aerodynamic model for model-based navigation on a delta-wing UAV-Reference-Cited by-同舟云学术

On the scalability of experimentally determined aerodynamic model for model-based navigation on a delta-wing UAV

Published:2023-06-19 Issue: Volume: Page:
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Container-title:2023 IEEE 10th International Workshop on Metrology for AeroSpace (MetroAeroSpace)
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Author:

Longobardi P.¹,Skaloud J.¹

Affiliation:

1. EPFL-CRYOS,Lausanne,Switzerland,CH-1015

Publisher

IEEE

Link

http://xplorestaging.ieee.org/ielx7/10189920/10189924/10189996.pdf?arnumber=10189996

Reference18 articles.

1. Quadrotor Inertial Navigation Aided by a Vehicle Dynamics Model with In-Flight Parameter Estimation;crocoll;Proceedings of the 27th International Technical Meeting of The Satellite Division of the Institute of Navigation (ION GNSS+ 2014),2014

2. Model-Aided Navigation for a Quadrotor Helicopter: A Novel Navigation System and First Experimental Results

3. Wind Estimation for a Quadrotor Helicopter in a Model-Aided Navigation System;müller;Saint Petersburg International Conference on Integrated Navigation Systems,2015

4. Integration of an Autopilot for a Micro Air Vehicle

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3. Identifying Aerodynamics of Delta-Wing Drones for Model-Based Navigation: A Comparative Study;IEEE Access;2024