Interplanetary trajectory Encke method FORTRAN program manual for the IBM system/360
Interplanetary trajectory Encke method FORTRAN program manual for IBM 360 computer
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Interplanetary trajectory Encke method FORTRAN program manual for IBM 360 computer
Spacecraft trajectory correction propulsion system
Heliocentric low thrust spacecraft trajectory analysis using two-variable asymptotic expansion method
Trajectory, guidance and environmental parameters and uncertainties effect on design optimization of out-of-orbit Viking soft lander
Apollo 11 lunar landing mission planning, control and evaluation of launch window and translunar, lunar parking orbit and transearth trajectories
Earth oblateness effects on lunar and interplanetary trajectories, using algorithm based on orbital elements variations
Hybrid patched conic technique as iterative procedure for generating translunar and transearth trajectories emphasizing computing time saving
Lawden primer vector theory applied to matched conic spacecraft trajectories optimization
Hybrid patched conic iterative technique for accurate moon-earth /transearth/ trajectory generation
Accelerated gradient projection method applied to rocket trajectory optimization for minimizing fuel required for placing payload in circular orbits
Planetary trajectory handbooks for mission and system analysis covering opportunities for Mercury, outer planets and Mars, contour charts, etc
Onboard moon-to-earth trajectory approach guidance with or without midcourse guidance using optical angular measurements
Coordinate systems generation for optimal trajectories, considering Lagrange multiplier as motion constant
Branched trajectory optimization for split rocket vehicles using projected gradient or steepest descent method
Perturbative effects of Jupiter moons on spacecraft flyby and postencounter heliocentric trajectories, noting precision targeting
Closed form solution for minimum fuel constant thrust trajectories for vehicle transfer in vacuum between arbitrary boundary conditions
Low thrust interplanetary swingby trajectories optimization, considering thrusting and coasting within sphere of influence
Pioneer-F Jupiter flyby mission planning, considering use of optimum broken plane trajectories to increase launch opportunity and/or payload capability