抄録
Since the launch of ADEOS satellite, it has been pointed out that the accuracy of the attitude data is very suspicious. Under such conditions, the estimation of satellite behavior was carried out utilizing RIS data, OCTS images, GCPs, etc.
This paper describes the method of the exterior orientation which treats the distance from the satellite to the geocenter, the longitude of the ascending node, orbit inclination and the argument of latitude as orientation parameters. Then the examinations concerning the satellite motion and attitude based on the method are introduced.
