Analysis of Rendezvous Radar Tracking Requirements for Angular Bias Compensation During Mission D
RENDEZVOUS POSSIBILITIES WITH THE IMPULSE OF OPTIMUM TWO-IMPULSE TRANSFER SPECIAL REPORT NO. 1
Laser Systems Research at Marshall Space Flight Center
Gemini - Guidance and control.
Analysis and design of space vehicle flight control systems. Volume VIII - Rendezvous and docking
Optimum Rendezvous Guidance Study Interim Report
Lunar excursion module mission and related guidance and control functions.
Shuttle Oft Level C Navigation Requirements
Guidance Strategies and Analysis for Low Thrust Navigation