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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.

Full text not available from this repository.


Item URL in elib:https://elib.dlr.de/30166/
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 AuthorsAuthor's ORCID iDORCID Put Code
Duda, H.UNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Krag, B.UNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Date:1995
Journal or Publication Title:Proceedings of 4 PWR-SNR Workshop "Full Envelope Agility", Eglin AFB, Florida, USA, 28 - 30 March 1995,
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
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: DLR-Beauftragter, elib
Deposited On:02 Apr 2006
Last Modified:27 Apr 2009 07:44

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