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SpacecraftAttitudeDynamicsanControl
- Spacecraft Attitude Dynamics and Control 航天器姿态控制的课件，十分难得；内容通俗易懂；十分完整；是从事航天研究的必须知识
C_newtyle
- 航天工程用轨道卡尔曼滤波器，姿态确定传感器组合为轨道罗盘+磁强计，是当前组合中最为常见的，适合于小型卫星-Kalman filter with orbital spaceflight, the orbital attitude determination sensor combination compass+ magnetometers, is currently the most common combination is suitable for small satellites
C_newtyle
- 航天常用姿态确定敏感器组合，太阳敏感器+速率陀螺+轨道罗盘，具体数据含义请参考章仁为的<《卫星姿态控制》>-Spacecraft attitude determination sensors commonly used in combination, sun sensor+ rate gyro compass+ tracks, the meaning of specific data please refer to Chapter Ren' s < " Satell
target_sat
- 本程序描述的是姿态四元数的积分求解过程，可用于航天航空以及机械领域。-This procedure is described in quaternion integral solution process can be used in aerospace and mechanical fields.
Attitude-Dynamics-
- 航天动力学的一个分支，研究航天器的姿态运动，包括航天器整体围绕其质心的运动以及航天器各部分之间的相对运动-A branch of space dynamics that studies the spacecraft s attitude movement, including the motion of the spacecraft as a whole around its centroids and the relative movement between the various part
ode45_linmod
- 荣格库塔姿态阶段，应用于航天领域，可以进行运算得出正确的姿态(The Carl Jung Kutta attitude phase, applied to the aerospace field, can be computed to obtain the correct attitude)
XIAOTUILI
- 近地遥感卫星，对地三轴稳定。 采用小推力器稳定系统。 轨道：500KM 太阳同步轨道； 形体：长宽高：1m 1m 2m； 质量：2 吨；（按均匀分布考虑） 小推力器选择：六对均为 5N， 控制精度：指向精度 0.1 度，稳定度 0.01 度/秒。(Stability simulation of spacecraft attitude small thruster)
MATLAB航天姿态控制仿真程序
- 航天器姿态控制仿真程序，利用simulink中sfunction方法建立航天器姿态动力学模型和运动学模型，利用linmod对非线性模型线性化。(The simulation program of spacecraft attitude control uses the sfunction method of Simulink to establish the dynamic model and kinematic model of spacecraft attitude, and uses li