Moormann, D. and Mosterman, P.J. and Looye, G. (1999) Object-oriented computational model building of aircraft flight dynamics and systems. Aerospace Science and Technology, 3 (3), pp. 115-126. ISSN 1270-9638.
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For economic reasons aircraft performance is pushed towards its physical limitations. As far as flight control is concerned, a thorough investigation of flight system dynamics is reqired, i.e., covering the interaction between flight dynamics (including airframe structural flexibility) and flight systems (consisting of actuators/motivators and controls). Computational handling of this interaction is best taken into account if a comprehensive simulation model is available within a common computer processable description. This paper describes the computational model building of such a multidisciplinary non-linear aircraft simulation model for the design and validation of flight control systems. The approach has been validated in several projects and is demonstrated in this contribution by various views on a common example. The object-oriented, equation-based software packace Dymola is used as the modelling environment.
|Title:||Object-oriented computational model building of aircraft flight dynamics and systems|
|Journal or Publication Title:||Aerospace Science and Technology|
|In ISI Web of Science:||Yes|
|Page Range:||pp. 115-126|
|Keywords:||object-oriented modeling, aircraft modelling, flight dynamics, aeroelasticity, flight systems, hybrid systems, Petri net, flight controls, model building, code generation|
|HGF - Research field:||Aeronautics, Space and Transport (old)|
|HGF - Program:||Aeronautics|
|HGF - Program Themes:||Aircraft Research|
|DLR - Research area:||Aeronautics|
|DLR - Program:||L AR - Aircraft Research|
|DLR - Research theme (Project):||L - Flexible Aircraft (old)|
|Institutes and Institutions:||Institute of Robotics and Mechatronics > Robotic Systems|
|Deposited By:||elib DLR-Beauftragter|
|Deposited On:||12 Nov 2007|
|Last Modified:||06 Jan 2010 16:28|
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