Process, methods and tools for flexible aircraft flight dynamics model integration
Process, methods and tools for flexible aircraft flight dynamics model integration
复制标题
柔性飞机飞行动力学模型集成的流程、方法和工具
DOI:
--
复制
发表时间:
2007
期刊:
影响因子:
--
通讯作者:
M. Reijerkerk
中科院分区:
文献类型:
--
作者:
T. Kier;G. Looye;Moriz Scharpenberg;M. Reijerkerk
Multi-disciplinary flight dynamics models for rigid and flexible aircraft are
used in various areas and stages of the aircraft design process, like for example flight loads
analysis and flight control law design. These models must be sufficiently accurate, but also
allow for thousands of simulations in a reasonable amount of time (i.e. ’loop-capable’).
Depending on the application, flight dynamics models need to be available in various
forms, like ODEs for nonlinear simulation, linear state space models for control analysis,
etc. A major challenge in development of multi-disciplinary flight dynamics models is
the handling and integration of data from various sources, removing overlaps, and filling
in gaps in case specific data is missing. During the last decade, the DLR Institute of
Robotics and Mechatronics has developed methods and tools for these tasks, as well as
for model implementation in various forms suitable for aircraft design analysis. Recently,
these aspects have been integrated in a standardized efficient model integration process,
called DAMIP (DLR Aircraft Model Integration Process). DAMIP uses the data structure
of VarLoads, which is developed in cooperation with Airbus, and is backed by appropriate
methods and tools. In this paper an overview of DAMIP will be given, as well as some
recent application examples.