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ADVANCES IN THE ASTRONAUTICAL SCIENCES
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Using the State-Dependent Riccati Equation and Kalman Filter Techniques to Design a Satellite Attitude Control Simulator (IAA-AAS-DyCoSS1-07-09)
By: Luiz C. G. de Souza and Victor M. R. Arena.
Pub. 2012, 14pgs.
PDF File. AAS 12-351.
Price: $29.00
 

Reprinted from Advances in the Astronautical Sciences Volume 145.

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