Rapid prototyping using inversion-based control and object-oriented modelling

被引:0
|
作者
Looye, Gertjan [1 ]
机构
[1] DLR German Aerospace Center, Institute of Robotics and Mechatronics, Oberpfaffenhofen, D-82234 Wessling, Germany
关键词
Control theory - Flight control systems - Flight dynamics - Rapid prototyping;
D O I
10.1007/978-3-540-73719-3_8
中图分类号
学科分类号
摘要
Object-oriented modelling allows for efficient construction of multi-disciplinary system models in a physically-oriented way. As a unique feature, the modelling approach allows for automatic generation of regular, static, as well as inverse simulation models. Inverse models form the basis of various commonly used nonlinear controller synthesis methods, such as Feedback Linearisation. The resulting multivariable control laws are easily tuned to meet performance specifications and avoid the need for gain scheduling. In combination with automatic inversion, these synthesis methods are ideally suited for control law rapid prototyping, allowing experimentation with command variables, control selection and allocation, etc. in very short automated design cycles. After selection of the final architecture, the control laws may be developed further in a detailed design stage. In this chapter, we demonstrate this approach on the aircraft-on-ground nonlinear control problem. © 2007 Springer-Verlag Berlin Heidelberg.
引用
收藏
页码:147 / 173
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