Support multi-satellite and multi-task real-time telemetry data reception, verification, de-framing and analysis functions, and telemetry channel information arrangement;
Support visual display of data in multiple forms such as tables, curves, charts, status lights, and drag-and-drop custom interface pages;
Support remote control command source code management, compilation and comparison, data retrieval, data block generation, encryption, verification and sending.
Cover all-element situation display from rocket launch, satellite in-orbit operation, ground equipment simulation, etc.;
Support the fine display of rocket stage separation, satellite attitude transformation, engine startup and other actions;
Support WebGL accelerated rendering, displaying the situation smoothly in common browsers, and complex navigation and data visualization.
Support constellation TT&C, formation, scheduling algorithm research, large-scale constellation scene simulation and status monitoring;
Support the dynamic display of constellation-to-earth beams and inter-satellite links, and the switching display of orbital inertial system/ground-fixed system;
Support tracking plan, satellite status, beam information, data flow, log and other information display functions.
Support orbit determination, orbit calculation, equipment scheduling, task planning, data statistics and other functions;
Support the planning and arrangement of multi-satellite TT&C, and the overall planning of TT&C equipment;
Support the display of tracking information, tracking plan, and statistical results in Gantt chart, curve, histogram and other ways;
Support the configuration of satellite and station information, and log service.
Construct a digital satellite twin system with multiple couplings of power, heat, light, electricity, magnetism and radiation;
Satellite-ground parallel simulation, supporting satellite and constellation status simulation, on-orbit operation, maintenance, and fault diagnosis.
Support precise model construction and calculation at the dynamics and kinematics level;
Support the design and simulation of typical satellite missions such as sub-satellite point trajectory keeping, descending node time keeping, orbit transfer;
Support the calculation of orbital control parameters in limited thrust mode, and output speed increment, start-up time, fuel consumption and other parameters;
Support the calculation of different modes of attitude, and the simulation of attitude maneuvering process.