Proceeding of the Twenty-Fourth Seminar on Space Flight and Guidance Theory Progress report no. 8, 1 Apr. - 31 Dec. 1965
Seminar on space flight and guidance theory, with special attention to mathematical solutions of system stability
CONFERENCE↗
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A supercircular entry guidance concept designed for maximum monitoring capability
Reentry vehicle guidance system for automatic or manual range control and with pilot monitoring capability
GUIDANCE SYSTEM↗
An analytical approach to solution of two- point boundary condition problems in optimal guidance Summary report, May 1965 - Apr. 1966
Analytical approaches to path-adaptive guidance functions, circular orbit trajectories, and use of Fortran-compiled programs
TRAJECTORY↗
Conference on guidance theory and trajectory analysis
Guidance theory and trajectory analysis conference - research goals and programs in celestial mechanics, astrodynamics, computer utilization, and optimizational calculations
ASTRODYNAMICS↗
Research in optimization and guidance theory
Trajectory optimization and guidance theory for powered flight vehicles
GUIDANCE AND CONTROL↗
Atmosphere reentry guidance - Return from the manned Mars mission.
Reentry guidance for manned Mars mission return considering capture and acceleration control, skip range and terminal range controls
ATTITUDE CONTROL↗
Unified guidance analysis in design of space trajectories.
Dimensionless differential corrections and proper coordinate system for generalized preflight guidance analysis
GUIDANCE AND CONTROL↗
The iterative guidance law for Saturn.
Iterative guidance law for Saturn launch vehicle for lunar landing, examining trajectory optimization
TRAJECTORY OPTIMIZATION↗
Requirements for onboard optical guidance of spacecraft on lunar trajectories.
Sensor requirements for midcourse guidance phase of spacecraft on lunar trajectories, with attention to optical measurements and statistical combining for trajectory estimates
OPTICAL MEASUREMENT↗
Simplified midcourse guidance techniques.
Six midcourse guidance techniques, noting Earth- Mars and Earth-Venus trajectory with small and large injection error
EARTH-MARS RENDEZVOUS TRAJECTORY↗
Piloted guidance and control of the Saturn V launch vehicle.
Man-machine system in control and guidance of Saturn V launch vehicle, emphasizing participation during atmospheric phase of flight profile
ROCKET INSTRUMENTATION↗
Guidance and control of the Mariner planetary spacecraft.
Guidance and control systems of Mariner planetary spacecraft, noting requirements, flight performance, systems configuration, etc
INTERPLANETARY NAVIGATION↗
Guidance and control in supercircular atmosphere entry.
Simulator results on guidance and control during supercircular atmospheric entry maneuvers
SPACE SIMULATOR↗
Analysis of surveyor midcourse guidance as a problem in the theory of maxima and minima.
Surveyor midcourse guidance treated by minima and maxima theory, noting terminal phase
SURVEYOR PROJECT↗
Digital simulation techniques for lunar midcourse guidance and navigation computer systems research.
Symbolic programming digital computer techniques, hardware interfacing and system errors in simulation of lunar midcourse guidance and navigation systems
NAVIGATION SYSTEM↗
Terminal guidance for continuous powered space vehicles.
Error correcting problem in space trajectory of continuous powered space vehicle, discussing optimal terminal guidance
ERROR CORRECTING DEVICE↗
Design considerations for Surveyor guidance
Design considerations for midcourse guidance and terminal descent system of Surveyor lunar soft landing spacecraft
LUNAR LANDING↗