A Reliable IPv6 Access and Transmission Method for Spaceborne Platforms Without Physical Ethernet Interfaces

With the development of space-based cloud computing and on-orbit intelligent processing, higher requirements have been imposed on standardized network interconnection for spaceborne platforms. However, constrained by size, power consumption, thermal design, and structural layout, some spaceborne platforms lack physical Ethernet interfaces and therefore cannot directly support standard Internet Protocol version 6 (IPv6) communications. In addition, harsh spaceborne operating conditions, including thermal-vacuum stress and potential radiation-induced disturbances, increase the risk of link anomalies, state inconsistency, and service interruption. To address these issues, this paper proposes a reliability-enhanced IPv6 access and transmission method for spaceborne platforms without physical Ethernet interfaces. On the processor side, a network TAP interface is established to reconstruct the semantics of a standard Layer-2 network device. Combined with a cooperative central processing unit–field-programmable gate array (CPU–FPGA) link-carrying mechanism, the proposed method enables transparent IPv6 access without modifying the native Linux protocol stack. To satisfy both standard spacecraft onboard network services and high-throughput engineering data transmission, a dual-channel architecture is designed, in which the service network channel is separated from the engineering data channel. In addition, a hierarchical reliability-oriented mechanism is constructed, consisting of hardware-level fault-tolerance design, reliable link interaction, status monitoring, and redundancy takeover. Experimental validation is conducted on a CPU-FPGA prototype platform under a thermal-vacuum environment and representative abnormal operating scenarios. The results show that the proposed method can stably support IPv6 address configuration, neighbor discovery, and end-to-end communication. Under zero-packet-loss conditions, the service network channel achieves an average stable throughput of 173.8 Mb/s, while the engineering data channel achieves a stable throughput of approximately 3.4 Gb/s. The system also demonstrates good service continuity during long-duration operation and under typical abnormal scenarios. The proposed method provides a verifiable system-level solution for realizing standardized IPv6 network access and reliability-enhanced data transmission on interface-constrained spaceborne platforms.