Author(s): Wang Guangmin
Pages: 44-50
Year: 1997 Issue:  4
Journal: Aerospace Control
Keyword:  Launch vehicle; Guidance system; Compensation;
Abstract: The real - time compensation methods to correct main errors of intertial units ofguidance system in launch vehicle during fligut is introduced. Orbit injecion accuracies ofsatellites is improved by using these methods. In this paper, taking inertial units of mediumaccuracy as example, compensation the to errors of launch vehicles is calculated.