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Analysis of Rotorcraft Pilot Couplings from the Flight Control System Modes Perspective

Autor: Yu, Y., Pavel, M. D., van Kampen, E. J., Masarati, P.

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=od______3731::e6c2e72150e103a2e976cc3627027dae
http://hdl.handle.net/11311/1112110

ROTORCRAFT-PILOT COUPLINGS: ANALYSIS AND DETECTION IN A SAFETY ENHANCEMENT FRAMEWORK

Autor: Fasiello, S., Yu, Y., Jump, M., Pavel, M. D., van Kampen, E. J., Masarati, P.

Publikováno v: Proceedings of the 44th European Rotorcraft Forum: Delft, The Netherlands, 2018
Proceedings of the 44th European Rotorcraft Forum

Nowadays, the complexity of high speed civil transport and highly-augmented rotorcraft, has led to an increase in the chances of encountering unwanted unstable phenomena, such as the so called Aircraft/Rotorcraft-Pilot Couplings (A/RPCs) or Pilot-Ind

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=dedup_wf_001::5cec8a39d960c147d057d57174079659

Adaptive spacecraft attitude control with incremental approximate dynamic programming

Autor: Ye Zhou, Kampen, E. -J, Chu, Q. P.

Publikováno v: 68th International Astronautical Congress, IAC 2017: Unlocking Imagination, Fostering Innovation and Strengthening Security, 11
Delft University of Technology
Scopus-Elsevier

This paper presents an adaptive control technique to deal with spacecraft attitude tracking and disturbance rejection problems in the presence of model uncertainties. Approximate dynamic programming has been proposed to solve adaptive, optimal contro

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=dedup_wf_001::6f2ac578846d168ea262085658648c24
http://resolver.tudelft.nl/uuid:00dbde19-b58d-4741-9735-8d01c718ec16

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