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Numerical State-Dependent Riccati Equation Approach for Missile Integrated Guidance Control

✍ Scribed by Vaddi, Sai; Menon, Padmanabhan K.; Ohlmeyer, Ernest J.


Book ID
120508477
Publisher
American Institute of Aeronautics and Astronautics
Year
2009
Tongue
English
Weight
298 KB
Volume
32
Category
Article
ISSN
0731-5090

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