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GUIDANCE-NAVIGATION CONTROL OBOUT ASCENT STAGE AND ORBITAL TRANSITION STAGE OF A SHUTTLE
Author(s): 
Pages: 14-21
Year: Issue:  4
Journal: Aerospace Control

Keyword:  Shuttle GuedanceNavigationReliability design~+Error modelRedundant technology;
Abstract: 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. Finally, it introduces reliability design aboutthe guidance-navigation system of the shutlle.
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