Accession Number : AD0633406

Title :   DETERMINATION OF THE TRAJECTORY OF A BODY, USING THE SECOND DERIVATIONS OF POTENTIALS,

Corporate Author : AERONAUTICAL CHART AND INFORMATION CENTER ST LOUIS MO LINGUISTIC SECTION

Personal Author(s) : Chulkov-Eyman,V. P.

Report Date : APR 1966

Pagination or Media Count : 7

Abstract : The press reports of recent years mention the attempts to use the earth's gravity field for the orientation of space ships. According to the published data, the attainable orientation accuracy is of an order of 1-2 min. As data units of different kinds, the control systems use the inertia systems which measure certain linear functions of second derivations of the potential. The accuracy of measurements amounts to 10 to the -4 of the measured value. In the present article it is shown that the measurement of the second derivations of potential can be used not only for the purposes of orientation, but also for the determination of a trajectory of the body. The demonstration is carried out with the aid of two idealized models. (Author)

Descriptors :   (*ORBITS, DETERMINATION), (*POTENTIAL THEORY, ORBITS), MODEL THEORY, USSR

Subject Categories : Geodesy
      Spacecraft Trajectories and Reentry

Distribution Statement : APPROVED FOR PUBLIC RELEASE