交会对接多航天器联合闭环测试模式设计与验证

Design and Verification of Joint Closed-loop Test Mode for Rendezvous and Docking Multiple Spacecraft

摘要:

在载人航天领域，多航天器交会对接技术是研制的关键和难题，闭环测试系统设计的重要性尤为突出，用于交会对接的多航天器联合闭环测试的设计与实施，实现了多航天器间的一体化实时动态同步电测，实现了多航天器及其测试系统的时序同步，以及敏感器及其模拟器和机电系统的动力学模型同步动态联合实时驱动的同步控制，采用了多航天器一体化实时精确控制的自动化测试，以及多航天器间多通道大回路信息流的实时统一管理。解决飞行任务阶段，多航天器交互状态的验证问题，在地面真实呈现交会对接飞行的全过程，达到多船器联合电测的目的。

Abstract:

In the field of manned spaceflight, multi spacecraft rendezvous and docking technology is the key and difficult problem of development, and the importance of the design of closed-loop test system is particularly prominent. The design and implementation of joint closed-loop test of multi spacecraft for rendezvous and docking realizes the integrated real-time dynamic synchronous electrical test of multi spacecraft, realizes the timing synchronization and sensitivity of multi spacecraft and its test system The dynamic model of the simulator and the mechanical and electrical system is driven synchronously and dynamically in real time. The automatic test of the integrated real-time precise control of multiple spacecraft and the real-time unified management of the multi-channel and large loop information flow between multiple spacecraft are adopted. To solve the problem of the verification of the interaction state of multiple spacecraft in the mission phase, and present the whole process of rendezvous and docking flight on the ground, so as to achieve the purpose of joint electrical measurement of multiple spacecraft.