DocumentCode
2976777
Title
System design with quality engineering
Author
Pohl, Ernst ; Robinson, Dave ; Jacobs, Jaff
Author_Institution
Dept. of Aeronaut. & Astronaut., USAF Inst. of Technol., Wright-Patterson AFB, OH, USA
fYear
1989
fDate
22-26 May 1989
Firstpage
1524
Abstract
The authors discuss the use of quality function deployment during the conceptual design of a kinesthetically controlled flight vehicle. Specifically, the techniques were used to increase the inherent dynamic stability of the vehicle through proper placement of critical components. The resulting design was robust to operator size and skill level as well as on-board weapon system and external-environment-induced oscillations. In the present work, particular emphasis is placed on parameter design, the goal of which is to take an organized approach to design tradeoffs so that the overall system performance is maximized while keeping costs at a minimum. Cost is incurred whenever the desired performance is not achieved. The identification of all applicable parameters that affect the performance of the system is discussed. The parameters fall into two broad classes: design parameters and noise parameters
Keywords
aircraft; design engineering; military equipment; quality control; design parameters; dynamic stability; external-environment-induced oscillations; kinesthetically controlled flight vehicle; noise parameters; on-board weapon system; parameter design; quality engineering; quality function deployment; system design; Aerospace engineering; Automotive engineering; Costs; Design engineering; Quality function deployment; Robustness; Stability; System performance; Vehicle dynamics; Weapons;
fLanguage
English
Publisher
ieee
Conference_Titel
Aerospace and Electronics Conference, 1989. NAECON 1989., Proceedings of the IEEE 1989 National
Conference_Location
Dayton, OH
Type
conf
DOI
10.1109/NAECON.1989.40418
Filename
40418
Link To Document