摘要: The NPSAT1 satellite uses an active magnetic torque rod system, with a magnetometer for attitude determination, to maintain 3-axis stabilization, with a slightly gravity gradient friendly structure, This thesis will examine the pe... 展开
作者 | Zirkle, T. A. | ||
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原报告号 | ADA397962 | 总页数 | 111 |
主办者 | Non Paid ADAS | ||
报告分类号 | [84D - Spacecraft Trajectories & Flight Mechanics] | ||
报告类别/文献类型 | AD / NTIS科技报告 | ||
关键词 | Magnetic fields Attitude control systems Satellite attitude Control Simulation Spacecraft Models Efficiency Theses Estimates Reduction Gravity Control theory Loops Switching Determination Torque Angular motion Gradients Attitude(Inclination) Magnetometers |