Trajectory optimization using regularized variables.
Trajectory optimization of space vehicle with continuous thrust based on regularized equations, comparing perturbation method for earth-Jupiter rendezvous transfer
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Trajectory optimization of space vehicle with continuous thrust based on regularized equations, comparing perturbation method for earth-Jupiter rendezvous transfer
Numerical integration for continuously thrusting spacecraft optimal trajectory, considering rectangular Cartesian and polar cylindrical coordinates characteristics
Closed form solution for minimum fuel constant thrust trajectories for vehicle transfer in vacuum between arbitrary boundary conditions
Vector integral extension to optimal trajectory coordinate multiplier systems with constant of motion demonstrated for coast-arc problem
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
Normalized hodographic mapping for constrained trajectory families, discussing mapping concepts, information content and applications
Trajectory analysis of multiplanet Grand Tour mission to four large outer planets on single flight, discussing mission planning
Apollo type reentry trajectory optimization numerical methods
Subroutines, logic, and input/output formats for STEP programs on preflight and postflight trajectory measurement
Cross wind effects on trajectory and cross section of turbulent jet
Numerical optimization of atmospheric reentry trajectories by sweep method
Optimal transfer trajectories from earth parking orbit to various terminal conic constraints, and ROBOT computer program modifications
Euler-Lagrange equations for approximating optimal thrust trajectories for limited hybrid propulsion system in N-body dynamic environment
Formulation on statistical trajectory estimation programs
Computer program for launch vehicle trajectory optimization
Mean orbital elements for Vinti spheroidal theory of drag-free satellite motion applied to ballistic trajectories