Title :
The research of flight reliability evaluation of missile
Author :
Xu, Ting-Xue ; Dong, Qi ; Zhang, Yong-Liang ; Zhao, Ya-Wen
Author_Institution :
Dept. of Ordnance Sci. & Technol., Naval Aeronaut. & Astronaut. Univ., Yantai, China
Abstract :
In this paper, the evaluation method for the flight reliability of missile has been proposed, for solving the problem that the small sample of missile flight experiment, mainly based on the maximum entropy method and the Bayes rules. We build up a flight reliability block diagram of missile and then discuss how to select the environmental factor during data integrated. The results show the feasibility of the proposed method.
Keywords :
Bayes methods; aerospace control; environmental factors; missile guidance; reliability; Bayes rules; block diagram; environmental factor; flight reliability evaluation; maximum entropy method; missile flight; Engines; Entropy; Environmental factors; Missiles; Reliability theory; Bayes; environmental factor; flight reliability; maximum entropy method; missile weapon system;
Conference_Titel :
Quality, Reliability, Risk, Maintenance, and Safety Engineering (ICQR2MSE), 2011 International Conference on
Conference_Location :
Xi´an
Print_ISBN :
978-1-4577-1229-6
DOI :
10.1109/ICQR2MSE.2011.5976724
