ORBITAL LAUNCH OPERATIONS. VOL. III- NAVIGATION, GUIDANCE AND RENDEZVOUS
Orbital launch operations - vol 3, navigation, guidance and rendezvous
MANNED SPACECRAFT↗
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PILOTED SIMULATION STUDIES OF RE-ENTRY GUIDANCE AND CONTROL AT PARABOLIC VELOCITIES
Piloted simulation studies of reentry guidance and control at parabolic velocities
VELOCITY↗
Control and Guidance of Electrically Propelled Spacecraft
Some of the conditions and methods of control and guidance for a nuclear-electric spacecraft are discussed in general terms. The type of spacecraft considered is propelled by an ion motor. The broad aspects of the flight trajectory peculiar to this type of propulsion are examined. Some equipment limitations are reviewed.
NUCLEAR-ELECTRIC PROPULSION↗
MULTIVARIABLE LINEAR FILTER THEORY APPLIED TO SPACE VEHICLE GUIDANCE
Multivariable linear filter theory applied to space vehicle guidance
SPACE VEHICLE↗
A SURVEY OF GUIDANCE AND NAVIGATION PROBLEMS FOR THE MANNED LUNAR MISSION
Guidance & navigation of manned lunar missions
MANNED SPACECRAFT↗
Analysis Of Guidance Perturbations For A Low-Thrust Mars Orbiter Mission Using Snap-8
Guidance perturbations for a low-thrust mars orbit mission using snap-8
SYSTEM FOR NUCLEAR AUXILIARY POWER-8 /SNAP-8/↗
THEORETICAL INVESTIGATION OF THE PERFORMANCE OF PROPORTIONAL NAVIGATION GUIDANCE SYSTEMS-EFFECT OF METHOD OF POSITIONING THE RADAR ANTENNA ON THE SPEED OF RESPONSE
Proportional navigation guidance systems - radar antenna positioning effects on speed of response
RADAR EQUIPMENT↗
A STUDY OF THE EFFECT OF A DEADBAND ABOUT A DESIRED PERIGEE ON THE GUIDANCE OF A SPACE VEHICLE APPROACHING THE EARTH
Guidance of spacecraft approaching earth at supercircular velocities on desired perigee
PERIGEE↗
INERTIAL GUIDANCE, ITS EVOLUTION AND FUTURE POTENTIAL
Space science - navigation - inertial guidance
NAVIGATION↗
GUIDANCE AND CONTROL SYSTEMS FOR SPACE CARRIER VEHICLES
Space science - launch vehicle and carrier rocket guidance-control systems
GUIDANCE SYSTEM↗
Progress Report No. 3 on Studies in the Fields of Space Flight and Guidance Theory
This paper contains progress reports of NASA-sponsored studies in the areas of space flight theory and guidance theory. The studies are carried on by several universities and industrial companies. This progress report covers the period from June 15, 1962 to December 20, 1962. The technical supervisor of the contracts is W.E. Miner, Deputy Chief of the Future Projects Branch of Aeroballistics Division, George C. Marshall Space Flight Center.
SPACECRAFT GUIDANCE↗
NUMERICAL APPROXIMATION OF MULTIVARIATE FUNCTIONS APPLIED TO THE ADAPTIVE GUIDANCE MODE PART II
Spacecraft guidance - numerical integration - computer method
NUMERICAL INTEGRATION↗
OPTIMAL MEASUREMENT AND VELOCITY CORRECTION PROGRAMS FOR MIDCOURSE GUIDANCE
Perturbation control for midcourse guidance in space trajectory program
SPACE TRAJECTORY PROGRAM↗
FINE GUIDANCE SENSOR FOR HIGH PRECISION CONTROL OF THE OAO
Guidance sensor for high precision control of oao needed when examining radiation from selected stars
GUIDANCE SENSOR↗
STUDIES IN THE FIELDS OF SPACE FLIGHT AND GUIDANCE THEORY. INTRODUCTION
Guidance systems and flight optimization theory for space flight
FLIGHT OPTIMIZATION↗
NUMERICAL APPROXIMATION OF MULTIVARIATE FUNCTIONS APPLIED TO THE ADAPTIVE GUIDANCE MODE
Numerical analysis of adaptive control systems - guidance systems
GUIDANCE SYSTEM↗
LINEAR PROGRAMMING APPLIED TO GUIDANCE FUNCTION FITTING
Linear programming for approximate computation of guidance function for adaptive control systems
LINEAR PROGRAMMING↗
A MINIMUM FUEL VERTICAL TOUCHDOWN LUNAR LANDING GUIDANCE TECHNIQUE
Minimum fuel vertical touchdown lunar landing guidance technique
FUEL CONSUMPTION↗