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