DocumentCode :
393637
Title :
Design of shape and control system for micro-airplane development
Author :
Ishikawa, H. ; Kajiwara, I. ; Yabe, Tatsuro
Author_Institution :
Tokyo Inst. of Technol., Japan
Volume :
1
fYear :
2002
fDate :
5-7 Aug. 2002
Firstpage :
599
Abstract :
In the field of airplane, technology for higher performance. miniaturization and lightening has been attracting the attention of the aircraft engineers. But the characteristic interference between the aerodynamics based on the structure shape and the control system can´t be ignored when the miniaturization is conducted. This papa demonstrates a design strategy of micro-airplanes by the use of simultaneous aerodynamic shape and control system optimization.
Keywords :
aircraft; control system synthesis; mobile robots; optimisation; micro-aeroplane development; micro-airplane control system design; micro-airplane shape design; Aerodynamics; Airplanes; Automotive engineering; Control systems; Equations; Laser feedback; Shape control; Stability; Vehicles; Vibration control;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
SICE 2002. Proceedings of the 41st SICE Annual Conference
Print_ISBN :
0-7803-7631-5
Type :
conf
DOI :
10.1109/SICE.2002.1195476
Filename :
1195476
Link To Document :
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