State-Dependent Riccati-Equation-Based Guidance Law for Impact-Angle-Constrained Trajectories
- 1 January 2009
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Guidance, Control, and Dynamics
- Vol. 32 (1), 320-326
- https://doi.org/10.2514/1.37876
Abstract
No abstract availableThis publication has 7 references indexed in Scilit:
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