Accession Number : AD0673134

Title :   ERROR ANALYSIS OF SINGLE AND TWO-FORCE FIELD SPACECRAFT ORBITS,

Corporate Author : GENERAL DYNAMICS/ASTRONAUTICS SAN DIEGO CALIF

Personal Author(s) : Ehricke,K. A.

Report Date : 22 SEP 1958

Pagination or Media Count : 55

Abstract : It is the purpose of astronautical error analysis to express mathematically the effect of errors or deliberate changes in velocity on the orbital elements of either transfer orbit or terminal orbit. (Author)

Descriptors :   (*ORBITS, MATHEMATICAL ANALYSIS), ERRORS, ELLIPTICAL ORBIT TRAJECTORIES, VELOCITY, AZIMUTH, TRANSFER TRAJECTORIES

Subject Categories : Numerical Mathematics
      Spacecraft Trajectories and Reentry

Distribution Statement : APPROVED FOR PUBLIC RELEASE