Výsledky vyhledávání - "Looye, Gertjan"

This paper presents a modelling scheme suitable for loads analysis of manoeuvres and gusts of a flexible controlled aircraft. In contrast to most ongoing research, the component to be investigated is not the wing but the vertical tail plane (VTP). Cr

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=od______1640::54a987f2423a5671bac6b34b95f3cb87
https://elib.dlr.de/128352/

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Design and Verification of a Linear Parameter Varying Control Law for a Transport Aircraft

Autor: Weiser, Christian, Ossmann, Daniel, Kuchar, Richard, Looye, Gertjan

This paper presents the design, implementation and simulator verification of inner loop control laws based on linear parameter varying controller design techniques for a CS-25 certified fly-by-wire test aircraft. The synthesis method provides, in con

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=od______1640::548382b4abe341df944f0d09d296d283
https://elib.dlr.de/127005/

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Flight testing of incremental backstepping based control laws with angular accelerometer feedback

Autor: Keijzer, Twan, Looye, Gertjan, Chu, Q. P., van Kampen, E.

Publikováno v: AIAA Scitech 2019 Forum: 7-11 January 2019, San Diego, California, USA
AIAA Scitech 2019 Forum

This paper discusses the design, implementation and flight testing of an incremental Backstepping (IBS) based manual flight control law with angular accelerometer (AA) feedback. The main advantages of incremental control laws are that they only requi

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=narcis______::2d8cf70f3f2dd9d490ac411b8c04cc4f
http://resolver.tudelft.nl/uuid:e4814409-24df-4a4f-9e9a-c03400e78ad7

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Recent Design and Flight Test Experiences with Nonlinear Control Methods

Autor: Kuchar, Richard, Looye, Gertjan

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=od______1640::c767a0bec52713f5c04cd305f5506add
https://elib.dlr.de/133012/

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Flight Tests on fault-tolerant autopilot control laws in laboratory aircraft Citation II

Autor: in 't Veld, A.C., Mulder, T.J., Looye, Gertjan H.N.

Publikováno v: Society of Flight Test Engineers-European Chapter Symposium

The Delft University laboratory aircraft Cessna Citation II has the capability to implement and test new auto pilot control laws. The aircraft is equipped as a Fly-By-Wire testbed, that enables the user to control the aircraft through an experimental

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=narcis______::deea0d9525de7830a72302b635ed335d
http://resolver.tudelft.nl/uuid:db2cf8d7-1535-4826-bd47-57f581395563

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Aircraft control using actuator current

Autor: van der Linden, Franciscus L. J., Looye, Gertjan, Pollack, Tijmen

From an actuation systems point of view, fly-by-wire aircraft are manoeuvred by controlling the position of the surfaces. In this paper, it is proposed to control the aircraft by the current through the electrical motors that move the surfaces. When

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=od______1640::8e9ca1771757ebfa280b3ab4f08aa4b7
https://elib.dlr.de/120314/

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