diagram stage
4.This paper analyses the guidance-navigation control device with its subsystemwhich is used in the ascent stage and the orbital transition stage of a shuttle, presents a methodused to choose data for a redundant system, describes the relationship between the configura-tion of afour-gimbal inertial platform and the attitude angle of a rocket, the error model ofthe instruments and its correction block diagram.
5.Then the dynamic characteristic of a last stage long blade with damped shroud is analyzed in detail,some results as untwist angle,static and dynamic frequency and Campbell diagram of nodal diameter vibration are obtained,the comparison of static frequency and dynamic frequency with results from three dimensional model shows the numerical model can get a rational result.

