An N-body low-thrust trajectory parameter optimization program, volume 3 Final report
Modifications to interplanetary trajectory program for providing capability of generating optimum low-thrust trajectory in N-body field
Engineering topics
Publications and source records attributed to Wolf, H..
Modifications to interplanetary trajectory program for providing capability of generating optimum low-thrust trajectory in N-body field
Interplanetary trajectory Encke method FORTRAN program manual for IBM 360 computer
Response of orbit determination systems to model errors
Orbit calculation using Encke perturbation method and Fortran IV programming
Set of uniform variational orbit parameters for space trajectory analysis
Convergence acceleration for least squares differential corrections
Space mission trajectory optimization by iterative minimizing of residual vector, using linear correction
Space mission trajectory optimization by iterative minimizing of residual vector, using linear correction
Quasilinear set of formulas developed for finite transformations
Modifications to minimum variance program for processing real data, including two-body problem solution, and modified Kalman filter with bias errors
Real time tracking & orbit prediction program for circular, elliptical, & hyperbolic orbits with perturbation forces