Author:
Lee Jaeho,Lee Yongwoo,Kim Youdan,Moon Gwanyoung,Jun Byung-Eul
Subject
Control and Systems Engineering
Reference4 articles.
1. Cimen, T. (2011). A Generic Approach to Missile Autopilot Design Using State-Dependent Nonlinear Control. 18th IFAC World Congress, Milano, Italy.
2. Mracek, C.P., and Cloutier J.R. (1997). Full Envelope Missile Longitudinal Autopilot Design Using the State-Dependent Riccati Equation Method. AIAA Guidance, Navigation, and Control Conference, New Orleans, LA.
3. Control Designs for the Nonlinear Benchmark Problem via the State-Dependent Riccati Equation Method;Mracek;International Journal of Robust and Nonlinear Control,1998
4. Numerical State-Dependent Riccati Equation Approach for Missile Integrated Guidance Control;Vaddi;AIAA Journal of Guidance, Control, and Dynamics,2009
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4 articles.
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