A Rule-Template-Based Simulation Method for Automatic Generation of Spacecraft TT&C Interface

Addressing the limitations of insufficient flexibility and efficiency bottlenecks inherent in traditional interface generation and simulation methods for spacecraft telemetry, tracking, and command (TT&C) systems, this paper presents a novel configuration architecture grounded in rule engine computation and modular template topology. The implementation of a dynamic rule parsing mechanism coupled with an extensible template framework facilitates autonomous orchestration and real-time adaptive rendering of interface elements. It effectively resolves critical issues including maintenance difficulties in hard-coded patterns and poor fault tolerance in pre-configured approaches. The system significantly enhances the response speed of human-machine interaction platforms in mission-intensive scenarios while supporting personalized demand customization for multi-position users. This technical solution provides reliable support for rapid deployment of complex aerospace missions.