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Analysis of a Magnetic Three-Axis Stabilized Attitude Control System for the NPSAT1 Spacecraft
Language: en
Pages: 111
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Type: BOOK - Published: 2001-09 - Publisher:

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The NPSAT1 satellite uses an active magnetic torque rod system, with a magnetometer for attitude determination, to maintain 3-axis stabilization, with a slightl
NPSAT1 Attitude Control Subsystem Hardware-in-the-Loop Simulation
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NPSAT1 is a three-axis stabilized spacecraft. Its Attitude Control Subsystem (ACS) uses a magnetic control approach that will be used for the first time. The Ma
Spacecraft Attitude Determination and Control
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Roger D. Werking Head, Attitude Determination and Control Section National Aeronautics and Space Administration/ Goddard Space Flight Center Extensiye work has
Design and Global Analysis of Spacecraft Attitude Control Systems
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