The multi-node efficient anti-interference communication method based on CCSDS protocol for Mars proximity space communication network

Lan Chen, Jia Tian, Aijun Zhang
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Abstract

Mars is the important goal in the exploration of the solar system. The maximum distance between Mars and earth is over 400 million kilometers, which means 22 minutes are needed for the earth station to transmit the telecommand to the spacecraft on Mars or receive the telemetry from them. Therefore, the real time control of the spacecraft on Mars is such a difficulty for earth station and a total automatic communication network is needed for orbiters and rovers themselves. The international common communication protocol for extraterrestrial planets is CCSDS proximity-1, which is widely used in various Mars probes of the United States, Europe and China. However, the CCSDS proximity-1 always operates between fixed pairs of spacecraft that usually belong to the same mission, which means the callers and the responders between these spacecraft are usually predefined, even when change is allowed, are pre-scheduled. For the possible hailing interferences from the spacecraft of other missions, the traditional method is “random back-off strategy”, which postpones the hailing process randomly when the failure of hailing is detected. The drawbacks are obvious: 1) the valuable communication time is wasted especially when the arc segment time is limited; 2) the random back-off cannot guarantee that the second time or third time will be successful; 3) the more the spacecraft of different missions are, the high the failure possibility is. In this paper, the multi-node efficient anti-interference communication method based on CCSDS protocol for Mars proximity space communication network is presented, which can monitor not only the return link, but also the side lobe of the forward link. Besides, the merging judgment mechanism is implemented in the data service sublayer of the CCSDS architecture, which can adjust the hailing process properly when the collision occurred and no extra time will be wasted. The method will be used in Chinese TW-3 probe. By using the conception products which simulate 5 orbiters and 5 rovers of different missions, real test shows that the presented method performs well in Mars proximity space communication network.
基于CCSDS协议的火星近地空间通信网络多节点高效抗干扰通信方法
火星是探索太阳系的重要目标。火星和地球之间的最大距离超过4亿公里,这意味着地球站向火星上的航天器发送远程指令或接收它们的遥测数据需要22分钟。因此,航天器在火星上的实时控制是地面站面临的一大难题,需要轨道飞行器和漫游者之间建立完全自动化的通信网络。国际上通用的地外行星通信协议是CCSDS proximity-1,广泛应用于美国、欧洲和中国的各种火星探测器。然而,CCSDS - proximi -1总是在通常属于同一任务的固定对航天器之间运行,这意味着这些航天器之间的呼叫者和响应者通常是预定义的,即使允许更改,也是预先安排的。传统的方法是“随机后退策略”,即在检测到呼叫失败的情况下,随机推迟呼叫过程。缺点很明显:1)浪费了宝贵的通信时间,特别是在弧段时间有限的情况下;2)随机退出不能保证第二次或第三次成功;3)不同任务的航天器数量越多,失效可能性越高。提出了一种基于CCSDS协议的火星近地空间通信网络多节点高效抗干扰通信方法,该方法不仅可以监测返回链路,还可以监测前向链路的旁瓣。此外,在CCSDS架构的数据服务子层中实现了合并判断机制,可以在发生碰撞时适当调整网约车进程,不会浪费额外的时间。该方法将用于中国的TW-3探测器。通过对不同任务的5个轨道飞行器和5个漫游者进行仿真,验证了该方法在火星近距离空间通信网络中的良好性能。
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