APPLICATION OF PONTRYAGIN'S MAXIMUM PRINCIPLE TO THE LUNAR ORBIT RENDEZVOUS PROBLEM
Time optimal control law for lunar orbit rendezvous validated by using the pontryagm principle
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Time optimal control law for lunar orbit rendezvous validated by using the pontryagm principle
Emergency rendezvous requirements of the apollo/ lem mission from a historical, nontechnical point of view
Two-impulse orbital transfer problem for elliptical orbits, describing techniques for finding optimum transfers and optimum rendezvous trajectories
Energy-optimal trajectories for terminal phase of satellite rendezvous
Astronaut role in spacecraft rendezvous, rescue, recovery and reentry systems design
Rendezvous capability of horizontal takeoff launch vehicle with air breathing propulsion system
Simulators for space rendezvous maneuver and docking
Optimal variable thrust rendezvous of power limited rocket between neighboring low eccentricity orbits
Gemini 6-Gemini 7 rendezvous photographs taken by Baker-Nunn camera
Gemini VI-A rendezvous mission planning, design criteria, and spacecraft trajectory
Computational method for two impulse orbital transfer and rendezvous between two elliptical orbits
Mathematical model using Euler-Lagrange equation to investigate liquid slosh effects on rendezvous dynamics
Linear theory of optimum variable thrust rendezvous trajectories with power limit propulsion system
Errors in Gemini rendezvous radar interferometer due to antenna ellipticity and coupling of adjacent antennas
Cassegrain monopulse tracking antenna for LEM and Command Module rendezvous guidance
Analysis of sextant navigation measurements during lunar module rendezvous
Simple feedback law for cooperative rendezvous problem
Optimal multiple impulse orbital rendezvous