Stabilization and real world satellite problemThe use of transformations of orbital equations has been considered in connection with requirements for more accurate data. The reported investigation is concerned with an evaluation of the relative merits of such transformations. The formulations tested include the classical Cowell formulation, the time regularized formulation, stabilization by the use of integrals, and stabilization by the use of elements. It is found that irrespective of efficiency considerations, stabilizing transformation makes it possible to obtain precisions which are unattainable with the Cowell formulations.
Document ID
19750060263
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Velez, C. E. (NASA Goddard Space Flight Center Greenbelt, Md., United States)