Development of a Hardware-In-Loop (HIL) Simulator for Spacecraft Attitude Control Using Momentum Wheels
نویسندگان
چکیده
منابع مشابه
Attitude Control Investigation Using Spacecraft Hardware-in-the-loop Simulator
The Distributed Spacecraft Attitude Control System Simulator (DSACSS) testbed at Virginia Polytechnic Institute and State University facilitates investigation of various control strategies for single and multiple spacecraft. DSACSS is comprised of two independent hardware-in-the-loop simulators and one software spacecraft simulator. The two hardware-in-theloop spacecraft simulators have similar...
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Virginia Tech has developed a testbed comprised of two independent spherical air-bearing platforms for formation flying attitude control simulation, the Distributed Spacecraft Attitude Control System Simulator (DSACSS). The DSACSS provides the flexibility to experimentally implement many types of control techniques. Novel individual platform control options include nonlinear compensation of an ...
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ژورنال
عنوان ژورنال: Journal of Astronomy and Space Sciences
سال: 2008
ISSN: 2093-5587
DOI: 10.5140/jass.2008.25.4.347