Minimum time aircraft trajectories between two points in range altitude space
Calculus of variations used to determine minimum time aircraft trajectories between two fixed points in range-altitude space
SEARCH · Search NASA
Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
Quote a phrase for an exact phrase match. Source license links do not imply unrestricted reuse.
Calculus of variations used to determine minimum time aircraft trajectories between two fixed points in range-altitude space
Celestial mechanics, astrodynamics, optimization theory, and onboard computations research for trajectory analyses of space flight vehicles
Research program on celestial mechanics for guidance and trajectory control application
Research scope in astrodynamics and computational methods for trajectory guidance theory, and procedures for mechanization
Nodal regression of orbit effect on gravity precession of gyroscopic satellite
Trajectory possibilities for Venus swingby mission and role in manned exploration of Mars
Trajectory characteristics of high-thrust Mars missions and effect on other aspects of mission planning
Iterative guidance mode with application to three- dimensional upper stage vacuum flight
Wind tunnel free-flight testing of reentry vehicle dynamics, noting capability for simultaneous two- dimensional viewing of model trajectories
Low-thrust trajectory requirements for solar system exploration using nuclear electric propulsion
Trajectory parameter determination in relation to various AROD airborne range and orbital determination ground stations
Two-variable asymptotic solution for three-dimensional solar powered low thrust trajectories in vicinity of ecliptic plane
General solutions to trajectory and orbit equations
Matched asymptotic expansion method applied to ordinary and optimal trajectory problems in hypervelocity flight dynamics
Periodic and almost periodic trajectories in cislunar space - techniques for determining behavior of dynamical systems of known periodic solutions, and space flight safety concept
Influence on trajectory determination of error in tracking station location and station time and frequency synchronization
Electric propulsion applied to lunar surface and Mars missions
Numerical calculation of three-dimensional trajectories using balanced horizontal and vertical motions