CAJ | 학술논문

为了达到保证气浮平台安全性和协助重心调节系统的目标，设计了一套基于三轴气浮台的卫星姿态物理仿真的举升控制系统，实现了对气浮台安全性和方便性能的改善。介绍了该举升控制系统的原理方案，对系统的总体结构进行了设计，以TMS320F2812为主控芯片设计了系统的硬件电路，其中主要包括各个模块的功能及系统的工作流程，进行了举升控制系统的软件算法设计。实验结果表明，该系统能够满足控制要求，实现了对性能的改善，具有响应快、精度高、可靠性强等特点，功能和指标都达到了设计要求。
위료체도보증기부평태안전성화협조중심조절계통적목표，설계료일투기우삼축기부태적위성자태물리방진적거승공제계통，실현료대기부태안전성화방편성능적개선。개소료해거승공제계통적원리방안，대계통적총체결구진행료설계，이TMS320F2812위주공심편설계료계통적경건전로，기중주요포괄각개모괴적공능급계통적공작류정，진행료거승공제계통적연건산법설계。실험결과표명，해계통능구만족공제요구，실현료대성능적개선，구유향응쾌、정도고、가고성강등특점，공능화지표도체도료설계요구。
In order to achieve the control goal of ensuring air-floating platform security and assisting gravity control system, the lifting control system of satellite attitude control system based on three-axis air-floating platform was designed to realize the improvement of the performance.Firstly, the principle and scheme of the lifting control system was presented. The overall structure of the system and the hardware circuit of the system was designed using TMS320F2812 as main control chip.It mainly consisted of the function of each module and the working process of the system.The software algorithm of the control system was presen-ted.With the experimental verification, the system met the control requirements and realized the improvement of the performance, and it also had advantages of fast response, high preci-sion and strong resistance to interference.The functions and indexes achieved the design re-quirements.