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AUTOMATIC GUIDANCE AND CONTROL FOR RENDEZVOUS
Error Analysis Apogee Biasing and Reference
An Exact ClosedForm Solution to the Rendezvous
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acceleration airlock analysis angle apogee approach approximately ascent astronaut attachment and connection attitude control body chaser closure phase components concept configuration constant control system coordinate system defined departure determined direction display docking maneuver Douglas Aircraft Company dynamic engine equations evaluation Figure flight ft/sec fuel function guidance hatch indicated inertia interception interceptor launch line-of-sight longitudinal engine Martin Company maximum method minimum mission mode module motion nominal obtained optimum orbital period orbital plane parameters parking orbit performance phase plane pilot position precession precession wheel pressure problem propulsion requirements propulsion system pulse radar range rate ratio relative velocity rendezvous maneuver rendezvous problem rendezvous vehicle rotating satellite sensor shown in Fig simulator Space Rendezvous space station space system space vehicle spacecraft spin axis subsystem target orbit target vehicle technique terminal thrust vector tion torque trajectory two-impulse variables velocity vector visual Vostok zero