Cross-platform spin-stabilized satellite flight simulation system

Abstract

The invention relates to a cross-platform spin stabilization satellite flight simulation system which mainly comprises a flight simulation control system and a dynamic simulation system. The flight simulation control system comprises an operation control module, a data transmitting module, a data receiving module, a remote control processing module, a monitoring display module and a real-time recording module. The dynamic simulation system mainly comprises a data input module, a four-stage engine ignition simulation module, a fuel amount / storage tank pressure and engine thrust computing module, an accelerometer nutation measured value computing module, an independent nutation control computing module, a nutation control / gesture control selecting module, a control force and torque computing module, a gesture kinematic and dynamic computing module, a control total impulse accumulation computing module and a track amount measurement computing module. The cross-platform spin stabilization satellite flight simulation system has relatively high versatility and can perform data exchange and simulated training with a spin stabilization satellite mold platform, a manned space flight satellite mold platform and an exploration satellite mold platform, thereby finishing simulation for states of satellite independent nutation control, rotating speed control, time delay measurement, gesture control, emergency nutation control, emergency spinning, etc.

Description

technical field [0001] The invention relates to a cross-platform spin-stabilized satellite simulation verification system, in particular to a cross-platform spin-stabilized satellite flight simulation system. The satellite simulation simulation software runs on the simulation computer of the measurement and control system, fully simulates various technical states of the satellite during flight, and completes the simulation of the satellite's autonomous chapter control, speed control, delay measurement, attitude control, emergency chapter control, emergency spin-up, etc. simulation. Background technique [0002] In the preparation process of the spin-stabilized satellite measurement and control mission, it is necessary to use the satellite measurement and control simulator to work with the shipborne measurement and control system to complete the satellite-ground large circuit drill, and to verify and verify the correctness and coordination of the software and hardware technic...

AI Technical Summary

Problems solved by technology

[0005] The technical problem to be solved by the present invention is to provide a cross-platform spin-stabilized satellite flight simulation system for the above-mentioned prior art, which adopts a high-level abstract and generalized data interface design, and solves the problems between the satellite flight simulation system and various satellite model platforms. It can be used as a highly versatile spin-stabilized satellite flight simulation system

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