A simulated study of manual control techniques for the concentrated flight plan of lunar orbit rendezvous - Project Apollo
Simulation of manual control techniques for concentric flight plan of LEM/CSM lunar orbit rendezvous
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Simulation of manual control techniques for concentric flight plan of LEM/CSM lunar orbit rendezvous
Rendezvous radar tracking requirements for angular bias compensation during Apollo 9 flight
Lunar module rendezvous using graphical charts
Lighting problem associated with terminal phase rendezvous in both earth and lunar orbit
Visibility and optical tracking studies for concentric flight plan of lunar orbit rendezvous
Apollo rendezvous with command module active for rescue of lunar module
CSM-active rendezvous simulation studies using sextant and ranging device
Range data requirements for CSM active rendezvous
Rendezvous procedures for lunar spacecraft
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Scanning laser radar system for automatic rendezvous and docking of space shuttle vehicles
Lunar module rendezvous with command and service module by coelliptic sequence establishing standard lighting and relative position and velocity for final approach
Time optimal rendezvous maneuver between neighboring elliptic orbits, discussing propulsive jet system with variable thrust
Manual spacecraft rendezvous system based on handheld instruments and manual computations, considering error analysis and simulation
Minimum-fuel multiple impulse orbital fixed time rendezvous in circular orbit vicinity
Future spacecraft mission for short period comets rendezvous, considering trajectory requirements and launch vehicle payload capabilities
Jupiter swingby trajectory analysis for comet flyby and rendezvous missions, discussing approach velocity and payloads
Manned Mars lander launch-to-rendezvous analysis, using subsequent Venus swingby for mission velocity requirement reduction