Abstract
The RCAM design challenge problem is defined in this chapter using two main sections. The first section discusses the basic flight dynamics model, the available inputs, outputs, parameters, etc. and the modelling of actuators, disturbances, etc. After that the control design specifications are given and the evaluation procedure to be performed by all design teams is presented.
The following authors contributed to the original RCAM design definition: Pierre Fabre, Joseph Irvoas, Philippe Ménard (Aerospatiale), Anders Helmersson (LiTH), Jean-François Magni (CERT), Tony Lambrecgts (DUT), Alberto MartÃnez (INTA), Stefano Scala (CIRA), Phillip Sheen (AVRO), Jan Terlouw (NLR) Hans van der Vaart (TU Delft).
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© 1997 Springer-Verlag
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Lambrechts, P., Bennani, S., Looye, G., Moormann, D. (1997). The RCAM design challenge problem description. In: Magni, JF., Bennani, S., Terlouw, J. (eds) Robust Flight Control. Lecture Notes in Control and Information Sciences, vol 224. Springer, Berlin, Heidelberg. https://doi.org/10.1007/BFb0113858
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DOI: https://doi.org/10.1007/BFb0113858
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