哈尔滨商业大学学报（自然科学版）Issue(1)：65-68,4.
基于三轴气浮台的卫星姿态控制系统物理仿真
Full physics simulation of satellite attitude control system based on three-axis air-floating platform
刘超 1何平 1李岐 1华楠1
作者信息
- 1. 哈尔滨工业大学航天学院控制科学与工程系，哈尔滨150001
- 折叠
摘要
Abstract
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.关键词
气浮台/物理仿真/举升控制/DSPKey words
air-floating platform/physical simulation/lifting control/DSP分类
信息技术与安全科学引用本文复制引用
刘超,何平,李岐,华楠..基于三轴气浮台的卫星姿态控制系统物理仿真[J].哈尔滨商业大学学报（自然科学版）,2015,(1):65-68,4.
