Title :
An integrated approach to robust avionics systems design
Author :
Pizzica, Stephen
Author_Institution :
Raytheon Co., El Segundo, CA, USA
Abstract :
Avionics equipment, particularly for military systems, must operate in harsh environments and satisfy strict reliability, test, and maintenance requirements. The design of avionics systems must therefore take these factors into account as well as meet the basic functional operational requirements. The methodology for ensuring that avionics equipment will operate reliably under all conceivable field conditions is known as robust design. To aid in meeting the various design objectives, extensive support tools have evolved in the commercial and military sectors. Examples of commonly used tools that are surveyed are: six sigma tools, DOE (Design of Experiments), sensitivity analysis, tolerance analysis, QFD (Quality Function Deployment), simulations, and checklists. It is shown that robust design factors need to be addressed as a whole rather than being considered separately. This paper advocates an integrated approach to robust avionics equipment design. In this approach, robust design is treated as a systems problem requiring a multi-objective design optimization.
Keywords :
avionics; design for manufacture; design for testability; design of experiments; life testing; military avionics; optimisation; quality management; reliability; safety; sensitivity analysis; tolerance analysis; DOE; HALT/HASS; checklists; design for reliability; design for safety; design for test; design of experiments; harsh environments; highly accelerated life test; highly accelerated stress screening; integrated approach; maintenance requirements; military systems; multi-objective design optimization; quality function deployment; reliability requirements; robust avionics systems design; sensitivity analysis; simulations; six sigma tools; tolerance analysis; Aerospace electronics; Maintenance; Military equipment; Quality function deployment; Robustness; Sensitivity analysis; Six sigma; System testing; Tolerance analysis; US Department of Energy;
Conference_Titel :
Digital Avionics Systems Conference, 2002. Proceedings. The 21st
Print_ISBN :
0-7803-7367-7
DOI :
10.1109/DASC.2002.1067965