Case study III: SA-330 PUMA (original) (raw)
Padfield, G.D. and Murray-Smith, D.J.(1991) Case study III: SA-330 PUMA. In: Rotorcraft System Identification. Series: AGARD advisory reports (280). AGARD: Neuilly sur Seine, France, pp. 176-212. ISBN 9789283506324
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Abstract
SA-330 Puma helicopter test data provided by the Royal Aerospace Establishment were analysed using a number of different identification techniques by six of the participating organisations in AGARD Flight Mechanics Panel Working Group WG-18. This section of the Report presents results of the six-degree-of-freedom identification, which are discussed in terms of the conventional rigid body modes of motion.
| Item Type: | Book Sections |
|---|---|
| Keywords: | Helicopter, system identification, parameter estimation, rigid-body model, Puma helicopter |
| Status: | Published |
| Glasgow Author(s) Enlighten ID: | Murray-Smith, Professor David |
| Authors: | Padfield, G.D., and Murray-Smith, D.J. |
| Subjects: | Q Science > QA Mathematics > QA75 Electronic computers. Computer scienceQ Science > QA Mathematics > QA76 Computer softwareT Technology > TJ Mechanical engineering and machineryT Technology > TK Electrical engineering. Electronics Nuclear engineeringT Technology > TL Motor vehicles. Aeronautics. Astronautics |
| College/School: | College of Science and Engineering > School of Engineering > Systems Power and Energy |
| Publisher: | AGARD |
| ISBN: | 9789283506324 |
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