Zobrazeno 1 - 10
of 64
pro vyhledávání: '"Coen C. de Visser"'
Autor:
Jasper J. van Beers, Coen C. de Visser
Publikováno v:
AIAA SciTech Forum 2023
Ensuring the reliability and validity of data-driven quadrotor model predictions is essential for their accepted and practical use. This is especially true for grey- and black-box models wherein the mapping of inputs to predictions is not transparent
Publikováno v:
AIAA SciTech Forum 2023
This paper proposes an extension to the traditional flight path reconstruction filter to simultaneously reconstruct the aircraft rigid body states together with modal amplitudes and velocities of the structure. To achieve this, the filter makes use o
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::43ed5048870bd0ddb417dd73e9649276
http://resolver.tudelft.nl/uuid:4f85c3f5-e885-4134-aa90-b36cd71a4eb5
http://resolver.tudelft.nl/uuid:4f85c3f5-e885-4134-aa90-b36cd71a4eb5
Publikováno v:
IEEE Transactions on Control Systems Technology. 29:2255-2263
Managing air data sensor fault detection and diagnosis (FDD) in the presence of atmospheric turbulence is challenging since the effects of faults and turbulence are coupled. Existing FDD approaches cannot decouple the faults from the turbulence. To a
Publikováno v:
IEEE Robotics and Automation Letters, 6(2)
Fault-tolerant control is crucial for safety-critical systems, such as quadrotors. State-of-art flight controllers can stabilize and control a quadrotor even when subjected to the complete loss of a rotor. However, these methods rely on external sens
Publikováno v:
Journal of Aerospace Information Systems. 18:14-25
In this paper, an online flight envelope protection system is developed and implemented on impaired aircraft with structural damage. The whole protection system is designed to be a closed loop of s...
Publikováno v:
AIAA SCITECH 2022 Forum
This paper proposes a new method that estimates the three-dimensional stochastic wind velocity for an aircraft equipped with a Pitot-static tube and airflow vanes. Since the performance of most state estimators, e.g., the extended Rauch-Tung-Striebel
Autor:
Prashant Solanki, Coen C. de Visser
Publikováno v:
AIAA SCITECH 2022 Forum
Quadcopters are becoming increasingly popular across diverse sectors. Since rotor damages occur frequently, it is essential to improve the attitude estimation and thus ultimately the ability to control a damaged quadcopter. This research is based on
Publikováno v:
AIAA SCITECH 2022 Forum
To gain more insight into human sensitivity to variations in simulated stall buffets, Just Noticeable Difference (JND) thresholds were estimated using a passive human-in-the-loop flight simulator experiment. Using an in-house developed flow separatio
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::b2e82ffbad833beb6811a0e5c157bc85
http://resolver.tudelft.nl/uuid:fec96ebf-a740-4758-93cc-419e3778fc9c
http://resolver.tudelft.nl/uuid:fec96ebf-a740-4758-93cc-419e3778fc9c
Publikováno v:
AIAA SCITECH 2022 Forum
Netherlands Aerospace Centre (NLR) and Delft University of Technology (TUD) have obtained an unmanned aerial vehicle to serve as a test platform for future aeroservoelastic flight testing. The purpose of this testbed is to collect data about flexible
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::de56a1a55b9d4a5517fab5824660e8ce
http://resolver.tudelft.nl/uuid:89b0b56f-4ffb-449c-9ec7-1b94e75bca18
http://resolver.tudelft.nl/uuid:89b0b56f-4ffb-449c-9ec7-1b94e75bca18
Autor:
Sihao Sun, Coen C. de Visser
Publikováno v:
IEEE Robotics and Automation Letters. 4:3868-3875
This letter presents a high-fidelity aerodynamic model of a quadrotor in the high-speed flight, with the normal configuration, or subjected to rotor failures. A novel experimental setup, data processing, and model identification procedure are develop