Title :
Optimal Design of Experiments for Identifying the Model Parameters of Gyroscope on a Centrifuge and Vibration Table Compound Test System
Author_Institution :
Xi´´an Res. Inst. of Hi-Tech
fDate :
Aug. 30 2006-Sept. 1 2006
Abstract :
Overloading and vibration compound test system which is combined by centrifuge and vibration table offers a new way for ground test to simulate flight. It is an important thing must be solved in the design of experiments for gyroscope under compound environment how to meet the requirement of linear acceleration and avoid influence of angle velocity of centrifuge. After analyzing the radius acceleration and confining condition of gyroscope in a centrifuge, a new design of combination plan is brought forward, which including regular octahedron six-point experiments, regular hexahedron eight-point experiments and round plane four-point experiments. The regression experiments of three factors two order quantic of gyroscope is realized by use of the centre combination design. It is shown in calculation that the new design of experiments reaches D-optimized criterion
Keywords :
acceleration; aerospace simulation; design of experiments; dynamic testing; gyroscopes; parameter estimation; regression analysis; vibrations; D-optimized criterion; centrifuge/vibration table; flight simulation; gyroscope; linear acceleration; model parameter identification; optimal design of experiments; overloading test system; radius acceleration; regression experiments; vibration table compound test system; Acceleration; Aerospace simulation; Cities and towns; Costs; Design methodology; Design optimization; Gyroscopes; Instruments; Parameter estimation; System testing;
Conference_Titel :
Innovative Computing, Information and Control, 2006. ICICIC '06. First International Conference on
Conference_Location :
Beijing
Print_ISBN :
0-7695-2616-0
DOI :
10.1109/ICICIC.2006.490