In Japan, several kinds of spacecraft are planned to use GPS receivers for position determination of spacecraft, and navigation. These spacecraft are OREX (Orbital Reentry Experiment Vehicle) and HOPE (H-II Orbiting P1anE), SFU (Space Flyer Unit), , VSOP (VLBI Space Observatory Programme) mission using MUSES-B (Mu Space Engineering Satellite-B), and Rendezvous/Docking mission in ETS-VII (Engineering Test Satellite-VII) project. Basically three kinds of GPS navigation systems, i.e. systems of, (1) GPS standalone navigation, (2) GPS-Inertial Measurement Unit (IMU) hybrid navigation, and (3) GPS differential/relative navigation, are applied to the Japanese spacecraft . Relation between the GPS navigations and the spacecraft depends on their orbits, required precisions, relative range, and so on. The required precisions of position and velocity range from 100 m to 1 m in position and from 10 cm/sec to 1 cm/sec in velocity. As a whole, it will be feasible for the Japanese spacecraft to satisfy the required precisions with use of various configuration of GPS navigation systems.
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