Computer Science
Scientific paper
Apr 1974
adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1974stin...7615222.&link_type=abstract
Unknown
Computer Science
Computer Programs, Coordinate Transformations, Orbit Calculation, Orbit Perturbation, Spacecraft Trajectories, Equations Of Motion, Three Body Problem, Variational Principles
Scientific paper
Computer programs for the calculation of orbits and partial derivatives are presented using regularized equations of motion and variational equations for the expression of spacecraft trajectories and their differential correction. The programs are based on the use of the Kustaanheimo-Stiefel coordinate transform with generalized eccentric anomaly as in dependent anomaly. The disturbing trajectory forces considered are earth asphericity, moon's attraction, and drag. They may be introduced in arbitrary combinations. The programs were developed on a CDC 6400/6500 computer using FORTRAN 4 in single precision.
No affiliations
No associations
LandOfFree
The utilization of regularized coordinates for the differential correction of spacecraft trajectories. Documentation of programs prepared in connection with the study does not yet have a rating. At this time, there are no reviews or comments for this scientific paper.
If you have personal experience with The utilization of regularized coordinates for the differential correction of spacecraft trajectories. Documentation of programs prepared in connection with the study, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and The utilization of regularized coordinates for the differential correction of spacecraft trajectories. Documentation of programs prepared in connection with the study will most certainly appreciate the feedback.
Profile ID: LFWR-SCP-O-813080