Study of lunar landing sensor performance interim report no. 1
Lunar landing sensor performance - characteristics of sensors for beacon and nonbeacon assistance
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Lunar landing sensor performance - characteristics of sensors for beacon and nonbeacon assistance
Lunar landing sensor performance - extended range altimeter, short range velocity sensor, and beacon tracking radar
Surveyor midcourse guidance treated by minima and maxima theory, noting terminal phase
Digital computer techniques applied to study of impact dynamics of lunar landing vehicles
Lunar navigation analysis using passive nongyro, inertial navigation, and radio frequency technology
Component capabilities and requirements for lunar navigation concepts
Modification of lunar landing research vehicle to lunar landing training vehicle
Advanced planetary missions using direct and relay link data return modes
Operational performance of electronic flight control system for lunar landing research vehicles
Surveyor midcourse guidance treated by minima and maxima theory, noting terminal phase
Concepts and calculations for lunar solar reflecting beacon designs to be used in Apollo mission
Flight test evaluation of on-off rate command attitude control system of manned lunar landing research vehicle
Computation procedure for motion of lunar landing vehicle during landing impact
Free flying lunar landing research vehicle tested for more than two years and used in lunar landing simulations supporting Apollo project
Ground and flight tests to evaluate lunar landing research vehicle fly-by-wire control system
LM guidance and control systems performance verification
Apollo lunar landing mission strategy development concerning guidance, control and landing and propulsion systems
Lunar landing trajectory, landing module electronics and Doppler radar, and probable landing sites modeled for ultrasonic simulation