Differential correction and preliminary orbit determination for lunar satellite orbits
Differential correction and preliminary orbit calculation for lunar satellite orbits
LUNAR SATELLITE↗
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Results for “Trajectory analysis”
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.
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Asteroid Belt and Jupiter flyby study Second bimonthly progress report, 15 Sep. - 30 Oct. 1964
Trajectory and mission analyses for asteroid belt and Jupiter flyby study
FLYBY MISSION↗
Virtual mass technique for computing space trajectories Final report
Virtual Mass Technique for computing spacecraft trajectories and Fortran IV computer program for related restricted three-body problem
SPACECRAFT TRAJECTORY↗
A calculation method for the ablation of glass-tipped blunt bodies
Trajectory and ablation characteristics calculation for glass-tipped blunt bodies in atmospheric entry
BLUNT BODY↗
New one-step integration methods of high accuracy
New numerical methods for solution of restricted three-body problem periodic trajectories and factors affecting accuracy and computer time through use of new methods
TRAJECTORY ANALYSIS↗
AS-202 launch vehicle operational flight trajectory
Launch vehicle operational flight trajectory for Saturn IB vehicle AS-202
SATURN IB LAUNCH VEHICLE↗
Study of structural bending adaptive control techniques for large launch vehicles Technical summary report, volume I
Application of spectral identification adaptive control system to large launch vehicle in complete closed loop trajectory simulation
ADAPTIVE CONTROL SYSTEM↗
Finite-thrust escape from and capture into circular and elliptic orbits
Finite-thrust escape and capture trajectories leading from circular or elliptic orbits to hyperbolic excess velocity vector located at gravitational sphere of influence
ESCAPE VELOCITY↗
Study of low-acceleration space transportation systems Summary report, Jul. 1964 - Jun. 1965
Feasibility of manned Mars mission using combined high and low thrust propulsion systems
TRAJECTORY ANALYSIS↗
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
TRAJECTORY ANALYSIS↗
Research goals and an integrated approach
Celestial mechanics, astrodynamics, optimization theory, and onboard computations research for trajectory analyses of space flight vehicles
SPACE FLIGHT↗
Research program for celestial mechanics
Research program on celestial mechanics for guidance and trajectory control application
GUIDANCE AND CONTROL↗
Research in astrodynamics and computer exploitation
Research scope in astrodynamics and computational methods for trajectory guidance theory, and procedures for mechanization
GUIDANCE AND CONTROL↗
The effects of the nodal regression of the orbit on the gravity precession of a gyroscopic satellite
Nodal regression of orbit effect on gravity precession of gyroscopic satellite
RELATIVITY THEORY↗
The Venus swingby mission mode and its role in the manned exploration of Mars.
Trajectory possibilities for Venus swingby mission and role in manned exploration of Mars
TRAJECTORY ANALYSIS↗
A survey of Mars mission trajectory characteristics.
Trajectory characteristics of high-thrust Mars missions and effect on other aspects of mission planning
SPACECRAFT TRAJECTORY↗
Development of the iterative guidance mode with its application to various vehicles and missions.
Iterative guidance mode with application to three- dimensional upper stage vacuum flight
EARTH-MOON TRAJECTORY↗
A wind tunnel free flight testing technique for nonplanar motion of spinning models.
Wind tunnel free-flight testing of reentry vehicle dynamics, noting capability for simultaneous two- dimensional viewing of model trajectories
TRAJECTORY ANALYSIS↗