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在宇航员完成在月面逗留之后,按照“阿波罗”计划考虑有登月舱的机动上升级与指挥服务舱的交会和对接。登月舱的上升级具有交会雷达,它是用于获得导引系统的输入参数,并用来监视和与应急导引系统一起工作。当出现需要保证援救登月舱上升级时,指挥服务舱必须变为可机动的宇宙飞行器。指挥服务舱的导引系统装有28倍放大率的六分仪,以及用于对接的,沿各固联轴定向的,刻有瞄准线的准直仪。利用登月舱上升级的光学瞄准来校正存储于宇航员舱的计算器内的相对位置向量。 “双子星座”计划的飞行试验表明,对于交会阶段而言,目标的亮度、飞行相位角和在末端由宇航员监视导引和减速过程在确定飞行器的控制性和交会所需要的推进剂裕量时是重要的。为了研究这些问题曾进行了在“阿波罗”船员舱内具有宇航员参加的相似——数字模拟试验,此时过渡的中心相位角为140°。特别研究了在宇宙飞行器位移加速度、相对位置向量信息的误差和在变化目标——追踪器高度差时为了交会所需的推进剂量之间的关系。 结论是在上述准则和对宇航员负担两种交会方案工作量的基础上确定的。在第一情况中,一位宇航员位于指挥服务舱内,并控制与登月舱上升级交会,而在第二种情况中,由3名宇航员在近地轨道上来实现与连接有登月舱的《土星——5
After the astronauts completed their stay on the lunar surface, they considered the rendezvous and docking of the maneuver upgrade of the lunar module with the command service module according to the “Apollo” plan. The lunar module is upgraded with a rendezvous radar, which is used to obtain the input parameters of the guidance system and to monitor and work with the emergency guidance system. The command service module must become a maneuverable spacecraft when there is a need to ensure that the rescue lunar module is upgraded. The guidance service cabin’s guidance system is equipped with a 28x magnification sextant and a collimator with line-of-sight collimators oriented along each solid-line axis for docking. Use the optical sightings upgraded on the lunar module to correct the relative position vectors stored in the calculator of the astronaut compartment. Flight tests conducted in the Gemini program show that for the rendezvous phase the brightness of the target, the phase angle of the flight, and the propellant margin required to determine the controllability and rendezvous of the aircraft at the end by the astronaut monitoring guidance and deceleration process When it is important. To study these issues, a similar-to-digital simulation of astronauts’ participation in the Apollo crew cabin was conducted, with a transitional center phase angle of 140 °. In particular, the relationship between the error of the spacecraft acceleration, the relative position vector information, and the propellant amount required for the rendezvous at the change target-tracker height difference was studied in particular. The conclusion is based on the above guidelines and on the workload of the astronauts on the two rendezvous programs. In the first case, an astronaut is located in the command service capsule and controls the rendezvous with the lunar module, while in the second case, three astronauts are on orbit with moon landing Cabin "Saturn - 5