Extracting physical tuning potentiometers from a complex control law - Application to flexible aircraft flight control

2001 ◽  
Author(s):  
Daniel Alazard
Keyword(s):  
Flight Control ◽  
Control Law ◽  
Flexible Aircraft ◽  
Complex Control ◽  
Aircraft Flight ◽  
Aircraft Flight Control

Modeling Study of Aircraft Based on Small Perturbation Equation

2012 ◽  
Vol 466-467 ◽  
pp. 1407-1412
Author(s):  
Du Wei Yang ◽  
Jian Zhong Zhou ◽  
Jun Chao Dong
Keyword(s):  
Flight Control ◽  
Complex Dynamics ◽  
System Modeling ◽  
Mathematics Model ◽  
Control Law ◽  
Perturbation Equation ◽  
Information Analysis ◽  
Aircraft Flight ◽  
Aircraft Flight Control ◽  
Output Information

In aircraft flight control law design, the first key is to establish actual aircraft mathematical model, then according to the model of dynamic output information, analysis control law design is appropriate. But in the movement the aircraft is a complex dynamics system, modeling is very complex. This paper firstly carry out comprehensive feasibility analysis, on a plane modeling consideration simplified, secondly, in actual applications verified using the perturbation method of nonlinear equation linearization, establish the plane mathematics model.

Advances in aircraft flight control

Automatica ◽  
2003 ◽  
Vol 39 (7) ◽  
pp. 1316-1319
Author(s):  
Andrew Sparks
Keyword(s):  
Flight Control ◽  
Aircraft Flight ◽  
Aircraft Flight Control
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