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首页> 外文期刊>Advances in Mechanical Engineering >A semi-physical simulation platform of attitude determination and control system for satellite:
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A semi-physical simulation platform of attitude determination and control system for satellite:

机译:卫星姿态确定与控制系统的半物理仿真平台:

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摘要

A semi-physical simulation platform for attitude determination and control system is proposed to verify the attitude estimator and controller on ground. A simulation target, a host PC, many attitude sensors, and actuators compose the simulation platform. The simulation target is composed of a central processing unit board with VxWorks operating system and many input/output boards connected via Compact Peripheral Component Interconnect bus. The executable programs in target are automatically generated from the simulation models in Simulink based on Real-Time Workshop of MATLAB. A three-axes gyroscope, a three-axes magnetometer, a sun sensor, a star tracer, three flywheels, and a Global Positioning System receiver are connected to the simulation target, which formulates the attitude control cycle of a satellite. The simulation models of the attitude determination and control system are described in detail. Finally, the semi-physical simulation platform is used to demonstrate the availability and rationality...
机译:提出了一种用于姿态确定和控制系统的半物理仿真平台,以验证地面上的姿态估计器和控制器。模拟平台由模拟目标,主机PC,许多姿态传感器和执行器组成。仿真目标由带有VxWorks操作系统的中央处理单元板和通过紧凑型外围组件互连总线连接的许多输入/输出板组成。目标的可执行程序是基于MATLAB的Real-Time Workshop从Simulink中的仿真模型自动生成的。一个三轴陀螺仪,一个三轴磁力计,一个太阳传感器,一个恒星示踪剂,三个飞轮和一个全球定位系统接收器被连接到模拟目标,从而制定了卫星的姿态控制周期。详细描述了姿态确定和控制系统的仿真模型。最后,使用半物理仿真平台来演示可用性和合理性。

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