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Prediction of PIO Susceptability of Highly Augmented Aircraft due to Rate Limiting Elements in Flight Control Systems.

Duda, H. and Krag, B. (1995) Prediction of PIO Susceptability of Highly Augmented Aircraft due to Rate Limiting Elements in Flight Control Systems. In: Proceedings of 4 PWR-SNR Workshop "Full Envelope Agility", Eglin AFB, Florida, USA, 28 - 30 March 1995,, pp. 302-315.

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Document Type:Conference or Workshop Item (Paper)
Additional Information: LIDO-Berichtsjahr=1995,
Title:Prediction of PIO Susceptability of Highly Augmented Aircraft due to Rate Limiting Elements in Flight Control Systems.
Authors:
AuthorsInstitution or Email of Authors
Duda, H.UNSPECIFIED
Krag, B.UNSPECIFIED
Date:1995
Journal or Publication Title:Proceedings of 4 PWR-SNR Workshop "Full Envelope Agility", Eglin AFB, Florida, USA, 28 - 30 March 1995,
Page Range:pp. 302-315
Status:Published
HGF - Research field:UNSPECIFIED
HGF - Program:Aeronautics
HGF - Program Themes:other
DLR - Research area:UNSPECIFIED
DLR - Program:L ST - Starrflüglertechnologien
DLR - Research theme (Project):UNSPECIFIED
Location: Oberpfaffenhofen
Institutes and Institutions:Institute of Flight Systems > Institut für Flugmechanik
Deposited By: elib DLR-Beauftragter
Deposited On:02 Apr 2006
Last Modified:27 Apr 2009 07:44

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