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
Full text not currently available from Enlighten.
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|
|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 science|
Q Science > QA Mathematics > QA76 Computer software
T Technology > TJ Mechanical engineering and machinery
T Technology > TK Electrical engineering. Electronics Nuclear engineering
T Technology > TL Motor vehicles. Aeronautics. Astronautics
|College/School:||College of Science and Engineering > School of Engineering > Systems Power and Energy|