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绘制自旋航天器的相平面图形,改变参数可以绘制不同情况下的姿态-Draw spacecraft spin phase planar graph, changing the parameters can be plotted attitude under different circumstances
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基于三轴航天器的姿态控制,按照实际情况,充分考虑了三轴的动力学和运动学耦合,能够单独控制各个角度姿态-Based on three-axis attitude control of the spacecraft, according to the actual situation, fully taking into account the dynamic and kinematic coupling triaxial, can be controlled separately for each
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用四元数为航天器设计的自适应滑模控制,可以实现航天器的姿态镇定-sliding mode control for spacecraft to stablize the attitude of spacecraft
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我们使用用欧拉角来表示航天器的姿态的仿真(Attitude simulation of Spacecraft Based on Euler angle)
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设置航天器敏感器或执行器故障,输出姿态角及角速度(set spacecraft fault of actuator or sensor,output attitude angle and attitude speed)
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用粒子群优化算法对三轴稳定航天器姿态控制PD参数进行自动寻优(optimization of PD parameter of attitude controller in spacecraft)
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姿态敏感器用来测量星体相对于某一基准方位的姿态信息,利用这些信息,可以确定星体的某一轴或三轴的姿态。星敏感器作为常用姿态敏感器,是以某一亮度高于+2可见星等的恒星为基准,测量其相对于航天器的角位置,并同星历表中的角位置参数进行比较,进而确定航天器的空间位置姿态。(The attitude sensor is used to measure the attitude information of a star relative to a certain datum direction. By us
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基于空间飞行器的姿态仿真程序-MATLAB源代码,给出姿态仿真结果(Spacecraft based attitude simulation program - MATLAB source code, gives attitude simulation results)
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