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- W2394028962 abstract "This paper puts forward the technique of reliability simulation for missile抯 flight control system under the influence of structural errors. The disturbance models of structural errors including missile mass asymmetry, different axis, airfoil fixed error and rudder null position are analyzed and established, and the distribution forms of structural errors random variables are assumed. The algorithm process and implementation approaches of reliability simulation are discussed in detail, and the formulas of computing reliability are given. The method is verified by X-missiles flight control system." @default.
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- W2394028962 date "2004-01-01" @default.
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- W2394028962 title "Study on Reliability Simulation for Flight Control System Considering Structural Errors" @default.
- W2394028962 hasPublicationYear "2004" @default.
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