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卫星姿态确定的卡尔曼滤波，使用matlab
仿真的姿态确定-satellite attitude determination
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通过卫星的测量方程和状态方程来求解卫星的姿态。包括四元数，角度，角速度等等。-By satellite measurements to solve equations and state equations of satellite attitude. Including the quaternion, angle, angular velocity and so on.
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简介卫星姿态控制系统的模型，并针对该模型分析故障发生的特点，故
障诊断的难点，以及可能发生故障的部位和故障的类型，给出故障检测的方法。-Introduction of satellite attitude control system model and the model for the analysis of the characteristics of faults, fault diagnosis of the difficulties, and possible failure l
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1.本程序是自己刚刚接触SAR时编写的时域星载SAR点目标回波仿真，包含了卫星轨道模型、计算星目斜距时用到的各种坐标系转换、SAR回波计算模型以及简单的SAR成像模型，希望对初学者有所帮助。
2.相应的参考资料可查找《卫星轨道姿态动力学与控制》及《魏钟铨_合成孔径雷达卫星》；-1. This program is just contact with their own prepared when the time domain SAR spaceborne SAR point target
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simulate multivariable system control.
Attitude Control of Spinning Satellite Subject to Actuators
Restriction Using EigenStructure Assignment.
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Aiming at determining the satellite attitude precisely，the gyros bias and m isa lignment were compensated in time by using the quaternion of star-sensor and extended Kalm an filter．The related module of the filter was derived．The theoretic accuracy o
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This satellite flight software
This is satellite attitude control system software-This is satellite flight software
This is satellite attitude control system software
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该程序完成了针对卫星姿态控制系统的执行器故障诊断和传感器故障诊断-The program has completed for the actuator fault diagnosis of satellite attitude control system and sensor fault diagnosis
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该程序描述了卫星姿态控制系统所需的欧拉角与四元数间的相互转换关系-The program required for satellite attitude control system is described the mutual conversion between euler angles and quaternions
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利用matlab simulink建立了卫星姿态控制系统模型，可以通过改变控制器等参数实现对卫星的控制-Satellite attitude control system was established based on the matlab simulink model, can be realized by changing the controller parameters, such as control of the satellite
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卫星姿态控制模型 用于控制算法的验证和仿真-Satellite attitude control model
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利用四元素的方法解算卫星姿态误差估计matlab程序代码-Satellite attitude error estimate
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利用四元素的方法解算卫星姿态误差估计的matlab程序源码-
The use of four elements method solver satellite attitude error estimation matlab Open Source
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Hoo/H2控制方法进行卫星姿态容错控制，包括卫星模型，控制器设计和参数文档-Hoo/H2 control method for satellite attitude fault-tolerant control, including satellite model, controller design and parameter document
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SimuLink仿真卫星姿态控制方法与案例，太完美了。-SimuLink simulation satellite attitude control methods and cases, too perfect.
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自动控制理论中卫星姿态控制系统，利用MATLAB画出已校正系统的单位阶跃和单位斜坡响应曲线。-The satellite attitude control system of automatic control theory is used to draw the unit step and slope response curve of the corrected system with MATLAB.
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卫星姿态是指卫星星体在轨道上运行所处的空间指向状态。将直角坐标系的原点置于星体上，指向地面的Z轴反映偏航方向，Y轴反映俯仰方向，X轴反映滚动方向。星体在高空中沿局部地球铅垂方向和轨道矢量方向运行，不时地产生对三轴的偏移。姿态控制是通过姿态控制分系统（ACS）来实现，使用地平扫描仪可感应俯仰和滚动轴的姿态误差，使用速度陀螺仪和罗盘可感应偏航轴的姿态误差。(Satellite attitude refers to the spatial orientation of a satellite in o
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attitude control of satellite with principal axes
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关于卫星姿态动力学的建模和姿态控制仿真，在code文件中(On the modeling and attitude control simulation of satellite attitude dynamics, in the code file)
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卫星姿态控制仿真，包括卫星轨道建模、卫星运动学、动力学建模，跟踪律计算(Satellite attitude control simulation, including satellite orbit modeling, satellite kinematics, dynamic modeling, tracking law calculation)
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