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An analytic solution of the state-dependent Riccati equation method for two-dimensional nonlinear systems is presented and the theoretical analysis of the missile longitudinal autopilot based on the SDRE method is performed using the analytic result.
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This page is a summary of: Analysis of Missile Longitudinal Autopilot Based on the State-Dependent Riccati Equation Method, Journal of Guidance Control and Dynamics, October 2019, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.g003679.
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